Browse

ftp://techreports.larc.nasa.gov (1075)

	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3307.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/phd-94-bey.ps.Z, 19950309 AN HP-ADAPTIVE DISCONTINUOUS GALERKIN METHOD FOR HYPERBOLIC CONSERVATION LAWS by KIM S. BEY, B.S., M.S. DISSERTATION Presented to the Faculty of the Graduate School of The University of Texas at Austin in Partial Fulfillment of the Requirements for the Degree of DOCTOR OF PHILOSOPHY THE UNIVERSITY OF
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/aiaa-93-3041.ps.Z, 19950309 1
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/cr189649.ps.Z, 19950309 Technical Report 77 April 1992 Computational Logic Inc. 1717 W. 6th St. Suite 290 Austin, Texas 78703 (512) 322-9951 This work was sponsored in part at Computational Logic, Inc. by National Aeronautics and Space Administration Langley Research Center (NAS1-18878). The views and conclusions contained in
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm4495.ps.Z, 19950309 NASA Technical Memorandum 4495 Pressure Distributions on a 0.02-Scale Space Shuttle Orbiter Nose at Mach 21.5 in Helium George C. Ashby, Jr., Peter T. Bernot, and William C. Woods January 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/cp3194-93-p277.ps.Z, 19950309 INTERIM REPORT OF THE METEOROID AND DEBRIS SPECIAL INVESTIGATION GROUP Michael E. Zolensky, Herbert A. Zook and Fred Horz SN2, NASA Johnson Space Center, Houston, TX 77058 Phone: 713/483-5129, FAX: 713/483-5347 Dale R. Atkinson, Cassandra R. Coombs and Alan J. Watts POD Associates Inc., 2309 Renard
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/conf-asnt-95-prosser.ps.Z, 19950309 1995 ASNT Spring Conference and Fourth Annual Research Symposium Las Vegas, Nevada, March 20-24, 1995 (A work of the US Government. Not subject to copyright by ASNT.) Detection and Location of Transverse Matrix Cracks in Cross-Ply Gr/Ep Composites Using Acoustic Emission W. H. Prosser K. E. Jackson S.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3208.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/tp3130.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm108986.ps.Z, 19950309 Single Block Three-Dimensional Volume Grids About Complex Aerodynamic Vehicles Stephen J. Alter Lockheed Engineering & Sciences Company, Hampton, Virginia and K. James Weilmuenstery NASA Langley Research Center, Hampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3454.ps.Z, 19950309 NASA Technical Paper 3454 Simultaneous Three-Dimensional Velocity and Mixing Measurements by Use of Laser Doppler Velocimetry and Fluorescence Probes in a Water Tunnel Dan H. Neuhart, David J. Wing, and Uleses C. Henderson, Jr. September 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3254.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/conf-53-nato-agard.ps.Z, 19950309 1 Situation Assessment in the Paladin Tactical Decision Generation System John W. McManus NASA Langley Research Center Hampton, Virginia Alan R. Chappell Lockheed Engineering and Sciences Company Hampton, Virginia P. Douglas Arbuckle NASA Langley Research Center Hampton, Virginia SUMMARY Paladin is a
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4351.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/conf-ieee-us-92-namkung.ps.Z, 19950309 AC MAGNETIC FIELD FREQUENCY DEPENDENCE OF MAGNETOACOUSTIC EMISSION M. Namkung, B. Wincheski , J. P. Fulton , and R. DeNale NASA Langley Research Center, Hampton, VA 23665 Analytical Services and Materials, Inc., 107 Research Dr., Hampton, VA 23666 Caderoc Division of Naval Surface Warfare Center,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm4562.ps.Z, 19950309 NASA Technical Memorandum 4562 Hypersonic Vehicle Model and Control Law Development Using H1 and Synthesis Irene M. Gregory, Rajiv S. Chowdhry, John D. McMinn, and John D. Shaughnessy October 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3426.ps.Z, 19950309 NASA Technical Paper 3426 CECOM Technical Report 93-B-E-3 Effective Declutter of Complex Flight Displays Using Stereoptic 3-D Cueing Russell V. Parrish, Steven P. Williams, and Dean E. Nold April 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm4564.ps.Z, 19950309 NASA Technical Memorandum 4564 Predicting Radiative Heat Transfer in Thermochemical Nonequilibrium Flow Fields Theory and User's Manual for the LORAN Code Lin Hartung Chambers September 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3408.ps.Z, 19950309 NASA Technical Paper 3408 Stochastic Solution to Quantum Dynamics Sarah John and John W. Wilson February 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3445.ps.Z, 19950309 NASA Technical Paper 3445 Effects of Isotope Selection on Solution Convergence in HZE Transport Myung-Hee Y. Kim, John W. Wilson, Richard L. Kiefer, and Sheila A. Thibeault May 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4382.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/rp1267.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/aiaa-95-0158.ps.Z, 19950309 Dual-Code Solution Strategy for Chemically-Reacting Hypersonic Flows William A. Wood NASA Langley Research Center, Hampton, VA 23681 and Scott Eberhardty University of Washington, Seattle, WA 98195
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/aiaa-95-6068.ps.Z, 19950309 1 American Institute of Aeronautics and Astronautics AIAA 95-6068 EXHAUST GAS MODELING EFFECTS ON HYPERSONIC POWERED SIMULATION AT MACH 10 Kenneth E. Tatum* Lockheed Engineering & Sciences Co. Hampton, Virginia and Lawrence D. Huebner NASA Langley Research Center Hampton, Virginia * Staff Engineer,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3291.ps.Z, 19950309 NASA Technical Paper 3291 CECOM Technical Report 92-E-5 December 1992 Scattering From Arbitrarily Shaped Microstrip Patch Antennas David G. Shively, Manohar D. Deshpande, and Capers R. Cockrell
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4338.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3225.ps.Z, 19950309 NASA Technical Paper 3225 ARL Technical Report 30 January 1993 Experimental and Analytical Investigation of Dynamic Characteristics of Extension-Twist-Coupled Composite Tubular Spars Renee C. Lake, Amir P. Izadpanah, and Robert M. Baucom
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/cr191509.ps.Z, 19950309 NASA Contractor Report 191509 A Formal Language for the Specification and Verification of Synchronous and Asynchronous Circuits David M. Russinoff COMPUTATIONAL LOGIC, INC. Austin, Texas Contract NAS1-18878 September 1993 NASA Contractor Report 191509 A Formal Language for the Specification and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/ijcse-4-4-6.ps.Z, 19950309 Computational Mechanics Analysis Tools for Parallel-Vector Supercomputers O. O. Storaasli , D. T. Nguyen , M. A. Baddourah*, and J. Qin Structures Division, Mail Stop 240, NASA Langley Research Center, Hampton VA 23681, U.S.A Center for Multidisciplinary Parallel-Vector Computation, Old Dominion
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm109109.ps.Z, 19950309 IMPLEMENTATION OF A VIBRATIONALLY LINKED CHEMICAL REACTION MODEL FOR DSMC Ann B. Carlson Langley Research Center, Hampton, VA and G. A. Bird GAB Consulting Pty Ltd, Australia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3419.ps.Z, 19950309 NASA Technical Paper 3419 Design and Evaluation of a Stochastic Optimal Feed-Forward and Feedback Technology (SOFFT) Flight Control Architecture Aaron J. Ostroff and Melissa S. Proffitt June 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm4588.ps.Z, 19950309 NASA Technical Memorandum 4588 Modeling of Instrument Landing System (ILS) Localizer Signal on Runway 25L at Los Angeles International Airport Richard M. Hueschen and Charles E. Knox November 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/aiaa-93-2915.ps.Z, 19950309 COMPUTER-AIDED LIGHT SHEET FLOW VISUALIZATION Kathryn Stacy, Kurt Severance*, and Brooks A. Childersy NASA Langley Research Center Hampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/aiaa-94-0219.ps.Z, 19950309 1 PARALLEL DSMC SOLUTION OF THREE-DIMENSIONAL FLOW OVER A FINITE FLAT PLATE Robert P. Nance* North Carolina State University, Raleigh, North Carolina Richard G. Wilmoth NASA Langley Research Center, Hampton, Virginia Bongki Moon University of Maryland, College Park, Maryland H. A. Hassan North Carolina
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3269.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/jpof-94-6-10.ps.Z, 19950309 Crossflow-Vortex Breakdown on Swept Wings: Correlation of Nonlinear Physics R. D. Joslin and C. L. Streett Theoretical Flow Physics Branch, Fluid Mechanics Division NASA Langley Research Center, Hampton, Virginia 23681
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4361.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/89/aiaa-89-3525.ps.Z, 19950309 APPLICATION OF ARTIFICIAL INTELLIGENCE (AI) PROGRAMMING TECHNIQUES TO TACTICAL GUIDANCE FOR FIGHTER AIRCRAFT John W. McManus and Kenneth H. Goodrich NASA Langley Research Center Mail Stop 489 Hampton, Virginia 23665-5225 (804)864-4037/(804)864-4009 AIAA Guidance, Navigation, and Control Conference
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4293.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3374.ps.Z, 19950309 NASA Technical Paper 3374 November 1993 Leading-Edge Vortex-System Details Obtained on F-106B Aircraft Using a Rotating Vapor Screen and Surface Techniques John E. Lamar, Jay Brandon, Kathryn Stacy, Thomas D. Johnson, Jr., Kurt Severance, and Brooks A. Childers
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm109078.ps.Z, 19950309 Comments Regarding Two Upwind Methods for Solving for Two-Dimensional External Flows Using Unstructured Grids William L. Kleb NASA Langley Research Center, Hampton, Virginia, 23681 Introduction Steady flow over the leading portion of a multicomponent airfoil section is studied us- ing computational
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3262.ps.Z, 19950309
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3466.ps.Z, 19950309 NASA Technical Paper 3466 Application of Two Procedures for Dual-Point Design of Transonic Airfoils Raymond E. Mineck, Richard L. Campbell, and Dennis O. Allison September 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/conf-tech2001-v2.ps.Z, 19950309 INCREASING PRODUCTIVITY THROUGH TOTAL REUSE MANAGEMENT (TRM) M. P. Schuler NASA Langley Research Center Hampton, VA 23665
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/tm4278.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4345.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4386.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3449.ps.Z, 19950309 NASA Technical Paper 3449 Optimal Control Theory Determination of Feasible Return-to-Launch-Site Aborts for the HL-20 Personnel Launch System Vehicle Kevin E. Dutton July 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3478.ps.Z, 19950309 NASA Technical Paper 3478 Navier-Stokes, Flight, and Wind Tunnel Flow Analysis for the F/A-18 Aircraft Farhad Ghaffari December 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3462.ps.Z, 19950309 NASA Technical Paper 3462 Experimental Validation of an Integrated Controls-Structures Design Methodology for a Class of Flexible Space Structures Peiman G. Maghami, Sandeep Gupta, Kenny B. Elliott, Suresh M. Joshi, and Joseph E. Walz November 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/aiaa-94-1579.ps.Z, 19950309 AIAA 94-1579flThermoelastic Formulation of Stiffened,flUnsymmetric Composite Panels for FiniteflElement Analysis of High Speed AircraftAIAA/ASME/ASCE/AHS/ACS fl35th Structures, Dynamics, & flMaterials ConferenceflApril 18-20, 1994/Hilton Head, SCCraig S. CollierflLockheed Engineering and Sciences
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/89/conf-rpqnde-9-89.ps.Z, 19950309 STRESS DEPENDENCE OF ULTRASONIC VELOCITY IN UNIDIRECTIONAL GRAPHITE/EPOXY COMPOSITES FOR LONGITUDINAL WAVES PROPAGATING ALONG THE DIRECTION OF STRESS William H. Prosser Mail Stop 231 NASA Langley Research Center Hampton, VA 23665 Review of Progress in Quantitative Nondestructive Evaluation, Vol. 9
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4410.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4302.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/90/aiaa-90-3435.ps.Z, 19950309 ARTIFICIAL INTELLIGENCE (AI) BASED TACTICAL GUIDANCE FOR FIGHTER AIRCRAFT John W. McManus Kenneth H. Goodrich NASA Langley Research Center Mail Stop 489 Hampton, Virginia 23665-5225 (804)864-4037/(804)864-4009 AIAA Guidance, Navigation, and Control Conference August 20-22, 1990 Portland, Oregon
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3455.ps.Z, 19950309 NASA Technical Paper 3455 Active Load Control During Rolling Maneuvers Jessica A. Woods-Vedeler, Anthony S. Pototzky, and Sherwood T. Hoadley October 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/agard-r-776.ps.Z, 19950309 1 DYNAMIC STALL EFFECTS AND APPLICATIONS TO HIGH PERFORMANCE AIRCRAFT by Jay M. Brandon NASA Langley Research Center Mail Stop 355 Hampton, Virginia 23665 SUMMARY This paper highlights recent research conducted at the NASA Langley Research Center on the effects of largeamplitude pitching motions on the
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/conf-rpqnde-93-p1809.ps.Z, 19950309 CHARACTERIZATION OF MAGNETOACOUSTIC EMISSION RELATED TO STRUCTURAL PROPERTIES OF FERROMAGNETS M. Namkung, B. Wincheski , J. P. Fulton and R. G. Todhunter NASA Langley Research Center Hampton, VA 23681 Analytic Services and Materials, Inc. 107 Research Dr., Hampton, VA 23666 INTRODUCTION An extensive
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/tp3112.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/conf-rpqnde-93-p1633.ps.Z, 19950309 AN APPLICATION OF A NEW ELECTROMAGNETIC SENSOR TO REAL-TIME MONITORING OF FATIGUE CRACK GROWTH IN THIN METAL PLATES M. Namkung, J. P. Fulton , B. Wincheski and C. G. Clendenin NASA Langley Research Center Hampton, VA 23681 Analytic Services and Materials, Inc. 107 Research Dr., Hampton, VA 23666
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4375.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/90/9-dasc.ps.Z, 19950309 A Concurrent Distributed System for Aircraft Tactical Decision Generation John W. McManus NASA Langley Research Center Hampton, Virginia 23665-5225
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm4533.ps.Z, 19950309 NASA Technical Memorandum 4533 Supersonic Aerodynamic Characteristics of a Circular Body Earth-to-Orbit Vehicle George M. Ware, Walter C. Engelund, and Ian O. MacConochie January 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm4601.ps.Z, 19950309 NASA Technical Memorandum 4601 Comparison of Computational and Experimental Results for a Supercritical Airfoil Melissa B. Rivers and Richard A. Wahls November 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/dmss.ps.Z, 19950309 NASA LANGLEY RESEARCH CENTER'S DISTRIBUTED MASS STORAGE SYSTEM Juliet Z. Pao D. Creig Humes MS157A NASA/Langley Research Center Hampton, VA. 23681
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/conf-18-icas.ps.Z, 19950309 AEROSPACE MEASUREMENTS: CHALLENGES AND OPPORTUNITIES Bruce A. Conway NASA Langley Research Center Hampton, Virginia 23665-5225
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3417.ps.Z, 19950309 NASA Technical Paper 3417 Local Performance Optimization for a Class of Redundant Eight-Degree-of-Freedom Manipulators Robert L. Williams II March 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3468.ps.Z, 19950309 NASA Technical Paper 3468 ARL Technical Report 480 Ten-Year Ground Exposure of Composite Materials Used on the Bell Model 206L Helicopter Flight Service Program Donald J. Baker September 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm107682.ps.Z, 19950309 Combined LAURA-UPS Hypersonic Solution Procedure William A. Wood and Richard A. Thompson Summary A combined solution procedure for hypersonic flowfields about blunted slender bodies has been implemented using a thin-layer Navier-Stokes code (LAURA) in the nose region and a parabolized Navier-Stokes code
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3164.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3168.ps.Z, 19950309
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3166.ps.Z, 19950309 Summary A robust closed-loop system" maintains desired stability and performance when the nominal system is subject to plant variations. Multivariable robustness analysis and robust control design tools take into account the uncertain nature of the plant models used in the design of feedback control
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm4548.ps.Z, 19950309 NASA Technical Memorandum 4548 Predicting the Effects of Unmodeled Dynamics on an Aircraft Flight Control System Design Using Eigenspace Assignment Eric N. Johnson, John B. Davidson, and Patrick C. Murphy June 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3242.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3425.ps.Z, 19950309 NASA Technical Paper 3425 A Mathematical Model for Simulating Noise Suppression of Lined Ejectors Willie R. Watson April 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/aiaa-95-0736.ps.Z, 19950309 11
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3429.ps.Z, 19950309 NASA Technical Paper 3429 Parallel Grid Generation Algorithm for Distributed Memory Computers Stuti Moitra and Anutosh Moitra February 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/cp3134-92-p459.ps.Z, 19950309 METEOROID & DEBRIS SPECIAL INVESTIGATION GROUP DATA ACQUISITION PROCEDURES Thomas H. See Martha K. Allbrooks Dale R. Atkinson Lockheed Engineering & Sciences Co. POD Associates, Inc. POD Associates, Inc. Houston, Texas 77058 Albuquerque, New Mexico 87106 Albuquerque, New Mexico 87106 (713)483-5027 / FAX
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3435.ps.Z, 19950309 NASA Technical Paper 3435 Tests of Highly Loaded Skids on a Concrete Runway Sandy M. Stubbs and Robert H. Daugherty March 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3234.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3469.ps.Z, 19950309 NASA Technical Paper 3469 Design Studies of Large Aperture, High-Resolution Earth Science Microwave Radiometers Compatible With Small Launch Vehicles Lyle C. Schroeder, M. C. Bailey, Richard F. Harrington, Bruce M. Kendall, and Thomas G. Campbell September 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3212.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3416.ps.Z, 19950309 NASA Technical Paper 3416 Computer-Aided Light Sheet Flow Visualization Using Photogrammetry Kathryn Stacy, Kurt Severance, and Brooks A. Childers July 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/tp3134.ps.Z, 19950309
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/conf-rpqnde-92-p1855.ps.Z, 19950309 CHARACTERIZATION OF ASYMMETRY IN MAGNETOACOUSTIC EMISSION BURST BY NUMERICAL PROCESSES M. Namkung NASA Langley Research Center Hampton, VA 23681 J. P. Fulton and B. Wincheski Analytic Services and Materials, Inc., Hampton, VA 23666 R. DeNale Caderoc Division of Naval Surface Warfare Center Annapolis, MD
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3235.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3284.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3375.ps.Z, 19950309 NASA Technical Paper 3375 December 1993 Structural Evaluation of Concepts for a Solar Energy Concentrator for Space Station Advanced Development Program Winfred S. Kenner and Marvin D. Rhodes
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/aiaa-93-3351.ps.Z, 19950309 1
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm4542.ps.Z, 19950309 NASA Technical Memorandum 4542 Effect of Leading- and Trailing-Edge Flaps on Clipped Delta Wings With and Without Wing Camber at Supersonic Speeds Gloria Hernandez, Richard M. Wood, and Peter F. Covell May 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/agard-94-803.ps.Z, 19950309 AGARD FDP/VKI Special Course on Optimum Design Methods for Aerodynamics von Karman Institute for Fluid Dynamics Rhode-Saint-Genese, Belgium 25-29 April 1994 AGARD Report 803 Airfoil Optimization by the One-Shot Method G. Kuruvila* ViGYAN, Inc. Hampton, VA 23666-1325 USA Shlomo Ta'asan Institute for
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4372.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/jtht-6-4-92-carlson.ps.Z, 19950309 RADIATION MODELING WITH DIRECT SIMULATION MONTE CARLO Ann B. Carlson* NASA Langley Research Center H. A. Hassan** North Carolina State University
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/jtht-7-2-93.ps.Z, 19950309 Radiation Transport Around Axisymmetric Blunt Body Vehicles Using a Modified Differential Approximation Lin C. Hartung NASA Langley Research Center, Hampton, VA 23665-5225 and H. A. Hassany North Carolina State University, Raleigh, NC 27695
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3437.ps.Z, 19950309 NASA Technical Paper 3437 The NASA Langley 8-Foot Transonic Pressure Tunnel Calibration Cuyler W. Brooks, Jr., Charles D. Harris, and Patricia G. Reagon August 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3360.ps.Z, 19950309 NASA Technical Paper 3360 September 1993 Wind Tunnel Investigations of Forebody Strakes for Yaw Control on F/A-18 Model at Subsonic and Transonic Speeds Gary E. Erickson and Daniel G. Murri
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/conf-rpqnde-92-p1071.ps.Z, 19950309 ANALYSIS OF THE MUTUAL INDUCTANCE BETWEEN TWO PARALLEL PLATES FOR THE DETECTION OF SURFACE FLAWS M. Namkung and C. G. Clendenin NASA Langley Research Center Hampton, VA 23681 J. P. Fulton and B. Wincheski Analytic Services and Materials, Inc., Hampton, VA 23666 INTRODUCTION There has recently been much
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3228.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4337.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/conf-asnt-1994-spring.ps.Z, 19950309 Accurate Simulation of Acoustic Emission Sources in Composite Plates Summary Paper for Presentation at 1994 ASNT Spring Conference New Orleans, March, 1994 W. H. Prosser M. R. Gorman NASA Langley Research Center Digital Wave Corporation MS 231 14 Inverness Drive East Hampton, VA 23681-0001 Building B,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/conf-hpc-95-p1.ps.Z, 19950309 Parallel Spatial Direct Numerical Simulation of Boundary-Layer Flow Transition on IBM SP1 Ulf R. Hanebutte 1 Ronald D. Joslin 2 Mohammad Zubair 3 1 Reactor Analysis Division Argonne National Laboratory Argonne, IL 60439 2 NASA Langley Research Center Hampton, VA 23681 3 International Business Machines
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4381.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm4563.ps.Z, 19950309 NASA Technical Memorandum 4563 Langley 14- by 22-Foot Subsonic Tunnel Test Engineer's Data Acquisition and Reduction Manual P. Frank Quinto and Nettie M. Orie June 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3253.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/conf-35-aace.ps.Z, 19950309 For presentation at the 1991 Conference of the American Association of Cost Engineers - 1 - Designing For Cost by Edwin B. Dean and Resit Unal THE MENTAL PROCESS OF DESIGNING FOR COST Designing for cost is a state of mind. Of course, a lot of technical knowledge is required and the use of appropriate
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm109025.ps.Z, 19950309 NASA TM 109025 (Revision 1) - 1 A Comparison of Queueing, Cluster and Distributed Computing Systems Joseph A. Kaplan (j.a.kaplan@larc.nasa.gov) Michael L. Nelson (m.l.nelson@larc.nasa.gov) NASA Langley Research Center June, 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3392.ps.Z, 19950309 NASA Technical Paper 3392 Experimental Studies of Transonic Flow Field Near a Longitudinally Slotted Wind Tunnel Wall Joel L. Everhart and Percy J. Bobbitt April 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/rp1281.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/conf-asnt-94-p125.ps.Z, 19950309 Classification of Magneto-Optic Images using Neural Networks Shridhar Nath, Buzz Wincheski and Jim Fulton Min Namkung Analytical Services and Materials Inc. NASA Langley Research Center 107 Research Drive Mail Stop 231 Hampton, VA 23666 Hampton, VA 23681 (804) 865-7093 (804) 864-4962 Magneto-Optic
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4295.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4309.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/rp1309.ps.Z, 19950309 NASA Reference Publication 1309 Small-Crack Effects in High-Strength Aluminum Alloys A NASA/CAE Cooperative Program J. C. Newman, Jr., X. R. Wu, S. L. Venneri, and C. G. Li May 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/aiaa-92-4026.ps.Z, 19950309 1 AIAA-92-4026 REYNOLDS NUMBER AND COWL POSITION EFFECTS FOR A GENERIC SIDEWALL COMPRESSION SCRAMJET INLET AT MACH 10: A COMPUTATIONAL AND EXPERIMENTAL INVESTIGATION by Scott D. Holland* NASA Langley Research Center Hampton, VA 23665
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/jtht-8-2-94.ps.Z, 19950309 Coupled Radiation Effects in Thermochemical Nonequilibrium Shock-Capturing Flowfield Calculations Lin C. Hartung, Robert A. Mitcheltree , and Peter A. Gnoffoy NASA Langley Research Center,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3205.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3460.ps.Z, 19950309 NASA Technical Paper 3460 DOT/FAA/RD-94/7 Microburst Vertical Wind Estimation From Horizontal Wind Measurements Dan D. Vicroy December 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4379.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/aiaa-93-0740.ps.Z, 19950309 1 AIAA-93-0740 AN EXPERIMENTAL PARAMETRIC STUDY OF GEOMETRIC, REYNOLDS NUMBER, AND RATIO OF SPECIFIC HEATS EFFECTS IN THREE-DIMENSIONAL SIDEWALL COMPRESSION SCRAMJET INLETS AT MACH 6 Scott D. Holland* and Kelly J. Murphy** NASA Langley Research Center Hampton, VA 23681
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3479.ps.Z, 19950309 NASA Technical Paper 3479 Kinetics Model for Initiation and Promotion for Describing Tumor Prevalence From HZE Radiation Francis A. Cucinotta and John W. Wilson December 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/conf-ieee-us-93-p753.ps.Z, 19950309 Self-organized Criticality and Phase Problem in Magnetoaocustic Emission Burst in Ferromagnets M. Namkung, J. P. Fulton and B. Wincheski NASA Langley Research Center, Hampton, VA 23681 Analytical Services and Materials, Inc., 107 Research Dr., Hampton, VA 23666
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3260.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3231.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/tp3114.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3232.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3438.ps.Z, 19950309 NASA Technical Paper 3438 Optical Position Measurement for a Large Gap Magnetic Suspension System Design and Performance Analysis Sharon S. Welch, James I. Clemmons, Jr., Kevin J. Shelton, and Walter C. Duncan June 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/90/jrpc-9-90.ps.Z, 19950309 Characterization of the Nonlinear Elastic Properties of Graphite/Epoxy Composites Using Ultrasound William H. Prosser and Robert E. Green, Jr. Journal of Reinforced Plastics and Composites, Vol. 9, March 1990, pp. 162-173
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/conf-asnt-94-p34.ps.Z, 19950309 Corrosion Detection in Airframes Using a New Flux-Focusing Eddy Current Probe James P. Fulton, Buzz Wincheski, and Shridhar Nath Min Namkung Analytical Services & Materials NASA Langley Research Center 107 Research Drive Mail Stop 231 Hampton, VA 23666 Hampton, VA 23681 (804) 865-7093 (804) 864-4962 A
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/cp3291-jones.ps.Z, 19950309 1 A GRID GENERATION SYSTEM FOR MULTI-DISCIPLINARY DESIGN OPTIMIZATION William T. Jones* Jamshid Samareh-Abolhassani** Computer Sciences Corporation, Hampton, Virginia 23666
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3202.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3221.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/aiaa-jsr-sep-oct-92.ps.Z, 19950309 A High Angle of Attack Inviscid Shuttle Orbiter Computation William L. Kleb and K. James Weilmuenstery NASA Langley Research Center, Hampton, Virginia, 23665 Introduction An accurate description of the aerothermal environment is required to minimize the weight of the Thermal Protection System required
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm4578.ps.Z, 19950309 NASA Technical Memorandum 4578 Numerical Aperture Limits on Efficient Ball Lens Coupling of Laser Diodes to Single-Mode Fibers With Defocus To Balance Spherical Aberration R. Gale Wilson November 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/cp3275-95-semres.ps.Z, 19950309 ANALYTICAL ELECTRON MICROSCOPY OF LDEF IMPACTOR RESIDUES Ronald P. Bernhard & Ruth A. Barrett Michael E. Zolensky Lockheed ESC, C-23 Solar System Exploration Division Johnson Space Center NASA Johnson Space Center Houston, Texas 77058 Houston, Texas 77058
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/rp1275.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/tm4305.ps.Z, 19950309
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/aiaa-93-2921.ps.Z, 19950309 For permission to copy or republish, contact the American Institute of Aeronautics and Astronautics 370 L Enfant Promenade, S.W., Washington, D.C. 20024 AIAA 93-2921 Interpretation of Waverider Performance Data Using Computational Fluid Dynamics Charles E. Cockrell, Jr. NASA-Langley Research Center
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/phd-91-prosser.ps.Z, 19950309 The Propagation Characteristics of the Plate Modes of Acoustic Emission Waves in Thin Aluminum Plates and Thin Graphite/Epoxy Composite Plates and Tubes by William H. Prosser NASA Technical Memorandum 104187 (November, 1991) A dissertation submitted to The Johns Hopkins University in conformity with the
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4366.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3219.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4453.ps.Z, 19950309 NASA Technical Memorandum 4453 X-15/HL-20 Operations Support Comparison W. Douglas Morris JUNE 1993
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/conf-rpqnde-92-fulton.ps.Z, 19950309 PRACTICAL ESTIMATES OF THE ERRORS ASSOCIATED WITH THE GOVERNING SHEAROGRAPHY EQUATION J. P. Fulton Analytical Services and Materials, Inc. 107 Research Drive Hampton, VA 23666 M. Namkung and L.D. Melvin NASA, Langley Research Center Hampton, VA 23681 INTRODUCTION In a series of papers Hung
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4380.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/aiaa-93-0192.ps.Z, 19950309 AIAA 93 0192 A COMPARISON OF THE PREDICTIVE CAPABILITIES OF SEVERAL TURBULENCE MODELS USING UPWIND AND CENTRAL-DIFFERENCE COMPUTER CODES Christopher L. Rumsey* and Veer N. Vatsa* NASA Langley Research Center Hampton, Virginia 23681 0001
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/conf-4-isaecm-92.ps.Z, 19950309 PROPAGATION OF FLEXURAL MODE AE SIGNALS IN GR/EP COMPOSITE PLATES W. H. Prosser and M. R. Gorman* MS 231 NASA Langley Research Center Hampton, VA 23665 (804) 864-4960 *Dept. of Aeronautics Naval Postgraduate School Monterey, CA 93943 (408) 646-2074 Proceedings of the Fourth International Symposium on
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3427.ps.Z, 19950309 NASA Technical Paper 3427 Subsonic Aerodynamic Characteristics of Semispan Commercial Transport Model With Wing-Mounted Advanced Ducted Propeller Operating in Reverse Thrust Zachary T. Applin, Kenneth M. Jones, Brenda E. Gile, and P. Frank Quinto July 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/conf-rpqnde-92-p1863.ps.Z, 19950309 FINITE ELEMENT MODELING OF THE BULK MAGNITIZATION OF RAILROAD WHEELS TO IMPROVE TEST CONDITIONS FOR MAGNETOACOUSTIC RESIDUAL STRESS MEASUREMENTS J. P. Fulton and B. Wincheski Analytical Services and Materials, Inc. 107 Research Drive Hampton, VA 23666 M. Namkung NASA, Langley Research Center Hampton, VA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/conf-13-ispa-unal+dean.ps.Z, 19950309 Presented at the 1991 Annual Conference of the International Society of Parametric Analysts. - 1 - TAGUCHI APPROACH TO DESIGN OPTIMIZATION FOR QUALITY AND COST: AN OVERVIEW Resit Unal Edwin B. Dean INTRODUCTION Calibrations to existing cost of doing business in space indicate that to establish human
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4317.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/ahsasc.ps.Z, 19950309 MULTILEVEL DECOMPOSITION APPROACH TO INTEGRATED AERODYNAMIC/DYNAMIC/STRUCTURAL OPTIMIZATION OF HELICOPTER ROTOR BLADES Joanne L. Walsh Katherine C. Young NASA Langley Research Center Hampton, Virginia Jocelyn I. Pritchard U. S. Army Vehicle Structures Directorate, ARL Hampton, Virginia Howard M. Adelman
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4333.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/cr187540.ps.Z, 19950309 Report on the Formal Specification and Partial Verification of the VIPER Microprocessor Bishop Brock Warren A. Hunt, Jr.1 Technical Report 46 January 15, 1990 Computational Logic, Inc. 1717 West Sixth Street, Suite 290 Austin, Texas 78703-4776 TEL: +1 512 322 9951 FAX: +1 512 322 0656 EMAIL:
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/cp3291-abolhassani.ps.Z, 19950309 GridTool: A Surface Modeling and Grid Generation Tool Jamshid Samareh-Abolhassani J.S.ABOLHASSANI@LaRC.NASA.GOV Computer Sciences Corporation NASA Langley Research Center Operation Geometry Laboratory (GEOLAB)
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4326.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/tm4313.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3270.ps.Z, 19950309 Summary Cockpit displays for a Takeo Performance Monitoring System (TOPMS) have been developed to provide pilots with graphic and alphanumeric information pertinent to their decision to continue or abort a takeoff. This information is presented to the pilots on panel-mounted head-down electronic display
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3256.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/conf-rpqnde-93-p1261.ps.Z, 19950309 LAMB WAVE RESPONSE OF FATIGUED COMPOSITE SAMPLES Reveiw of Progress in Quantitative Nondestructive Evaluation, Vol 13B (1994) pp. 1261-1266 Michael D. Seale and Barry T. Smith Departments of Physics and Applied Science The College of William and Mary Williamsburg, VA 23187 William H. Prosser Mail Stop
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3387.ps.Z, 19950309 NASA Technical Paper 3387 Numerical and Experimental Analyses of the Radiant Heat Flux Produced by Quartz Heating Systems Travis L. Turner and Robert L. Ash March 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4371.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3329.ps.Z, 19950309 NASA Technical Paper 3329 Constrained Minimization of Smooth Functions Using a Genetic Algorithm Daniel D. Moerder and Bandu N. Pamadi November 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3467.ps.Z, 19950309 NASA Technical Paper 3467 CECOM Technical Report 94-E-1 Spatial Awareness Comparisons Between Large-Screen, Integrated Pictorial Displays and Conventional EFIS Displays During Simulated Landing Approaches Russell V. Parrish, Anthony M. Busquets, Steven P. Williams, and Dean E. Nold October 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3452Vol3.ps.Z, 19950309 NASA Technical Paper 3452 Volume 3 HiRel: Hybrid Automated Reliability Predictor (HARP) Integrated Reliability Tool System (Version 7.0) HARP Graphics Oriented (GO) Input User's Guide Salvatore J. Bavuso, Elizabeth Rothmann, Nitin Mittal, and Sandra Howell Koppen November 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4296.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/aiaa-92-2951.ps.Z, 19950309 Characteristics of the Shuttle Orbiter Leeside Flow During A Reentry Condition William L. Kleb and K. James Weilmuenster y NASA Langley Research Center, Hampton, Virginia, 23665
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tt10001.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/conf-ttc-93-p369.ps.Z, 19950309 LARGE-EDDY SIMULATION OF BOUNDARY LAYER TRANSITION ON SWEPT WINGS Xiaoli Huai, Department of Mechanical Engineering University of Maryland College Park, MD 20742 Ronald D. Joslin Theoretical Flow Physics Branch NASA Langley Research Center Hampton, VA 23681 and Ugo Piomelli 1 Department of Mechanical
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4319.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/conf-rpqnde-11-92.ps.Z, 19950309 NONLINEAR ELASTIC EFFECTS ON THE ENERGY FLUX DEVIATION OF ULTRASONIC WAVES IN GR/EP COMPOSITES Review of Progress in Quantitative NDE, Vol. 11 (1992) pp. 2041-2048. William H. Prosser M.S. 231 NASA Langley Research Center Hampton, VA 23665 R. D. Kriz E.S.M., Norris Hall Virginia Tech. Blacksburg, VA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/aiaa-95-0737.ps.Z, 19950309 1 Nomenclature freestream Mach number p static pressure (psia) freestream pressure (psia) freestream Reynolds number s arc length along model surface measured radially from the dome/axisymmetric centerline intersection (in) Xbody streamwise distance along body (see Fig. 4) (in) a angle of attack (deg)
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4362.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3211.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm107708.ps.Z, 19950309 EFFECT OF SONIC BOOM ASYMMETRY ON SUBJECTIVE LOUDNESS By Jack D. Leatherwood and Brenda M. Sullivan SUMMARY The NASA Langley Research Center's sonic boom apparatus was used in an experimental study to quantify subjective loudness response to a wide range of asymmetrical N-wave sonic booms signatures.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3236.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3158.ps.Z, 19950309 Nomenclature A amplitude of Tollmien-Schlichting wave am;k Landau coefficient governing growth of Tollmien-Schlichting wave B amplitude of Dean vortex bm;k Landau coefficient governing growth of Dean vortex f nondimensional steady-state streamwise-velocity distri bution gm;k Landau coefficient governing
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/cr4527.ps.Z, 19950309 A.1. Using Hybrid mjrty 67 The other lemma states that if all good processors vote for a nonerror value, and all manifest-faulty processors vote for an error value, then the sum of the cardinalities of good, arbitrary, and symmetric faulty processors is at least as large as the value returned by count
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3446.ps.Z, 19950309 NASA Technical Paper 3446 High-Alpha Research Vehicle (HARV) Longitudinal Controller: Design, Analyses, and Simulation Results Aaron J. Ostroff, Keith D. Hoffler, and Melissa S. Proffitt July 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/tp3146.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3188.ps.Z, 19950309 Summary A multiaxis thrust-vectoring nozzle designed to have equal flow-turning capability in pitch and yaw was conceived and experimentally tested for internal static performance at Langley Research Center. The cruciform-shaped, convergent-divergent nozzle turned the flow for thrust vectoring by
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/tp3476.ps.Z, 19950309 NASA Technical Paper 3476 Internal Aerodynamics of a Generic Three-Dimensional Scramjet Inlet at Mach 10 Scott D. Holland January 1995
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/tp3113.ps.Z, 19950309
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4384.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm107764.ps.Z, 19950309 SUBJECTIVE RESPONSE TO SIMULATED SONIC BOOMS WITH GROUND REFLECTIONS by Brenda M. Sullivan and Jack D. Leatherwood SUMMARY The Sonic Boom Simulator at NASA Langley Research Center was used to (1) quantify subjective loudness of simulated composite sonic booms, each of which was comprised of a simulated
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3224.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3453.ps.Z, 19950309 NASA Technical Paper 3453 Estimates of Cellular Mutagenesis From Cosmic Rays Francis A. Cucinotta and John W. Wilson July 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4385.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm109120.ps.Z, 19950309 NASA Technical Memorandum 109120Modeling of Aircraft Unsteady Aerodynamic Characteristics Part 1 - Postulated ModelsVladislav Klein and Keith D. NodererThe George Washington University, Joint Institute for Advancement of Flight Sciences, Langley Research Center, Hampton, VirginiaMay 1994National
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3246.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3472.ps.Z, 19950309 NASA Technical Paper 3472 Extension of the BRYNTRN Code to Monoenergetic Light Ion Beams Francis A. Cucinotta, John W. Wilson, and Francis F. Badavi November 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/89/conf-33-aace.ps.Z, 19950309 - 1 - PARAMETRIC COST ANALYSIS: A DESIGN FUNCTION By Edwin B. Dean NASA Langley Research Center Transaction of the American Association of Cost Engineers 33rd Annual Meeting San Diego CA 25-28 June 1989 Parametric cost analysis uses equations to map measurable system attributes into cost. The measures
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/conf-asnt-94-p105.ps.Z, 19950309 Detection of Cracks at Welds in Steel Tubing Using Flux Focusing Electro- magnetic Probe Buzz Wincheski, Jim Fulton and Shridhar Nath Analytical Services and Materials 107 Research Drive Hampton, VA 23666 804 865-7093 John Simpson Min Namkung Lockheed Engineering & Sciences Co. Mail Stop 231 144
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/conf-ieee-us-92-p825.ps.Z, 19950309 MULTI-MODE EXCITATION AND DATA REDUCTION FOR FATIGUE CRACK CHARACTERIZATION IN CONDUCTING PLATES B. Wincheski , M. Namkung, J.P. Fulton , and C.G. Clendenin NASA Langley Research Center, Hampton, VA 23681 Analytical Services and Materials, Inc., 107 Research Dr., Hampton, VA 23666
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4390.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/jtht-6-3-92.ps.Z, 19950309 Stagnation Point Nonequilibrium Radiative Heating and the Influence of Energy Exchange Models Lin C. Hartung, Robert A. Mitcheltree , and Peter A. Gnoffoy NASA Langley Research Center, Hampton, VA 23665-5225
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/jtcfd-93-4-6.ps.Z, 19950309 Spatial Direct Numerical Simulation of Boundary-Layer Transition Mechanisms: Validation of PSE Theory R.D. Joslin and C.L. Streett NASA Langley Research Center, Hampton, VA 23681 and C.-L. Chang High Technology Corporation, Hampton, VA 23666 Abstract. A study of instabilities in incompressible
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3197.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3452Vol2.ps.Z, 19950309 NASA Technical Paper 3452 Volume 2 HiRel: Hybrid Automated Reliability Predictor (HARP) Integrated Reliability Tool System (Version 7.0) HARP Tutorial Elizabeth Rothmann, Joanne Bechta Dugan, Kishor S. Trivedi, Nitin Mittal, and Salvatore J. Bavuso November 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm107746.ps.Z, 19950309 A LABORATORY STUDY OF SUBJECTIVE RESPONSE TO SONIC BOOMS MEASURED AT WHITE SANDS MISSILE RANGE by Brenda M. Sullivan and Jack D. Leatherwood SUMMARY The Sonic Boom Simulator of the Langley Research Center was used to quantify subjective loudness response to boom signatures consisting of: (a) simulator
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/conf-rpqnde-91-p1213.ps.Z, 19950309 APPLICATION OF GUIDED ACOUSTIC WAVES TO DELAMINATION DETECTION Keun J. Sun* Department of Physics College of William and Mary Williamsburg, VA 23185 INTRODUCTION The occurrence of delamination in laminate structures is one of the major reliability concerns for using these materials. There are continuing
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/90/conf-17-icas.ps.Z, 19950309 ICAS-90-2.2.1 NASA Programs in Advanced Sensors and Measurement Technology for Aeronautical Applications Bruce A. Conway NASA Langley Research Center Hampton, Virginia 23665-5225
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/aiaa-joa.ps.Z, 19950309 GRID SENSITIVITY AND AERODYNAMIC OPTIMIZATION OF GENERIC AIRFOILS Ideen Sadrehaghighiy Old Dominion University, Norfolk, Virginia 23529-0247 Robert E. Smithz NASA Langley Research Center, Hampton, Virginia 23681-0001 Surendra N. Tiwarix Old Dominion University, Norfolk, Virginia 23529-0247
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/cr189704.ps.Z, 19950309 Formal Verification of an Oral Messages Algorithm for Interactive Consistency1 John Rushby Computer Science Laboratory SRI International Menlo Park CA 94025 USA Rushby@csl.sri.com Phone: +1 (415) 859-5456 Fax: +1 (415) 859-2844 Technical Report CSL-92-01 July 1992 1This research was supported by the
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm109038.ps.Z, 19950309 NASA Technical Memorandum 109038 Intel NX to PVM3.2 Message Passing Conversion Library Trey Arthur Computer Sciences Corporation Hampton, Virginia and Michael Nelson National Aeronautics and Space Administration Langley Research Center Hampton, Virginia October 1993 National Aeronautics and Space
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/aiaa-93-3966.ps.Z, 19950309 - 1 - Why Does It Cost How Much Edwin B. Dean * NASA Langley Research Center Hampton VA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm4582.ps.Z, 19950309 NASA Technical Memorandum 4582 Experimental Study at Low Supersonic Speeds of a Missile Concept Having Opposing Wraparound Tails Jerry M. Allen and Carolyn B. Watson November 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/cr4386.ps.Z, 19950309 Mechanical Verification of a Generalized Protocol for Byzantine Fault Tolerant Clock Synchronization Reprint from J. Vytopil, editor: Formal Techniques in Real-Time and FaultTolerant Systems, Nijmegen, The Netherlands, January 1992, pages 217{236; Volume 571 of Springer Verlag Lecture Notes in Computer
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3473.ps.Z, 19950309 NASA Technical Paper 3473 Performance Study of Galactic Cosmic Ray Shield Materials Myung-Hee Y. Kim, John W. Wilson, Sheila A. Thibeault, John E. Nealy, Francis F. Badavi, and Richard L. Kiefer November 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3440.ps.Z, 19950309 NASA Technical Paper 3440 Two-Dimensional Converging-Diverging Rippled Nozzles at Transonic Speeds John R. Carlson and Scott C. Asbury July 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/cp3194-93-p339.ps.Z, 19950309 3-D CRATER ANALYSIS OF LDEF IMPACT FEATURES FROM STEREO IMAGERY Clyde A. Sapp and Thomas H. See Lockheed Engineering & Sciences Co., Houston, TX 77058 Phone: 713/483-5141, FAX: 713-483-5347 Michael E. Zolensky SN2/NASA, Johnson Space Center, Houston, TX 77058 Phone: 713/483-5128, FAX: 713-483-5347
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3210.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/conf-nurbs.ps.Z, 19950309 TRIANGULATION OF NURBS SURFACES Jamshid Samareh-Abolhassani
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3136.ps.Z, 19950309
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/aiaa-92-4145.ps.Z, 19950309 1 A High-Fidelity Batch Simulation Environment for Integrated Batch and Piloted Air Combat Simulation Analysis Kenneth H. Goodrich* and Dr. John W. McManus** NASA Langley Research Center, Hampton Virginia Alan R. Chappell Lockheed Engineering & Sciences Company, Hampton Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/tm109170.ps.Z, 19950309 NASA Technical Memorandum 109170 Volume I NASA Langley Scientific and Technical Information Output\|1994 Marilou S. Phillips and Susan H. Stewart, Compilers January 1995
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/conf-ieee-us-93-p673.ps.Z, 19950309 QUALITY FACTOR AND MICROSLIPPING OF FATIGUE CRACKS IN THIN PLATES AT RESONANT VIBRATION B. Wincheski , M. Namkung, and J.P. Fulton NASA Langley Research Center, Hampton, VA 23665 Analytical Services and Materials, Inc., 107 Research Dr., Hampton, VA 23666
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/phd-92-mcmanus.ps.Z, 19950309 DESIGN AND ANALYSIS TECHNIQUES FOR CONCURRENT BLACKBOARD SYSTEMS A Dissertation Presented to The Faculty of the Department of Computer Science The College of William and Mary in Virginia In Partial Fulfillment of the Requirements for the Degree of Doctor of Philosophy by John William McManus ii APPROVAL
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm4567.ps.Z, 19950309 NASA Technical Memorandum 4567 Electronic Document Distribution: Design of the Anonymous FTP Langley Technical Report Server Michael L. Nelson and Gretchen L. Gottlich March 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/aiaa-93-3454.ps.Z, 19950309 UNSTRUCTURED GRIDS ON NURBS SURFACES Jamshid Samareh-Abolhassani
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/aiaa-95-0964.ps.Z, 19950309 THE WIDEST PRACTICABLE DISSEMINATION: THE NASA TECHNICAL REPORT SERVER Michael L. Nelson and Gretchen L. Gottlich NASA Langley Research Center, Hampton, Virginia David J. Bianco Computer Sciences Corporation/NASA Langley Research Center, Hampton, Virginia Robert L. Binkley and Yvonne D. Kellogg NASA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/rp1325.ps.Z, 19950309 NASA Reference Publication 1325 Mission Description and In-Flight Operations of ERBE Instruments on ERBS and NOAA 10 Spacecraft February 1987 Through February 1990 Kathryn A. Bush and Keith T. Degnan November 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm4559.ps.Z, 19950309 NASA Technical Memorandum 4559 Oxidation Performance of Platinum-Clad Mo-47Re Alloy Ronald K. Clark and Terryl A. Wallace June 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3171.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3229.ps.Z, 19950309 NASA Technical Paper 3229 September 1992 Open-Loop Characteristics of Magnetic Suspension Systems Using Electromagnets Mounted in a Planar Array Nelson J. Groom and Colin P. Britcher
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/aiaa-91-3209.ps.Z, 19950309 For permission to copy or republish, contact the American Institute of Aeronautics and Astronautics 370 L Enfant Promenade, S.W., Washington, D.C. 20024 AIAA 91-3209 Generic Hypersonic Inlet Module Analysis Charles E. Cockrell, Jr. Lawrence D. Huebner NASA-Langley Research Center Hampton, VA AIAA 9th
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3448.ps.Z, 19950309 NASA Technical Paper 3448 Baseline Tests of an Autonomous Telerobotic System for Assembly of Space Truss Structures Marvin D. Rhodes, Ralph W. Will, and Coung Quach July 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3209.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3245.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/aiaa-95-0478.ps.Z, 19950309 AIAA 95 0478 Airfoil Design and Optimization by the One-Shot Method G. Kuruvila ViGYAN, Inc., Hampton, VA Shlomo Ta'asan Carnegie Mellon University, Pittsburgh, PA M.D. Salas NASA Langley Research Center, Hampton, VA 33rd Aerospace Sciences Meeting and Exhibit January 9-12, 1995 / Reno, NV Airfoil
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4374.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3395.ps.Z, 19950309 NASA Technical Paper 3395 Effects of Expected-Value Information and Display Format on Recognition of Aircraft Subsystem Abnormalities Michael T. Palmer and Kathy H. Abbott March 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3257.ps.Z, 19950309 NASA Technical Paper 3257 March 1993 Static and Aerothermal Tests of a Superalloy Honeycomb Prepackaged Thermal Protection System Mark P. Gorton, John L. Shideler, and Granville L. Webb
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/cr4384.ps.Z, 19950309 Formal Specification and Verification of a Fault-Masking and Transient-Recovery Model for Digital Flight-Control Systems1 John Rushby Computer Science Laboratory SRI International Menlo Park CA 94025 June 19, 1991 1This research was supported by NASA Langley Research Center under contract NAS1 18969
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4359.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3451.ps.Z, 19950309 NASA Technical Paper 3451 En Route Noise Levels From Propfan Test Assessment Airplane Donald P. Garber and William L. Willshire, Jr. September 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/jasa-96-2.ps.Z, 19950309 1 PLATE MODE VELOCITIES IN GRAPHITE/EPOXY PLATES W. H. Prosser and M. R. Gorman* MS 231 NASA Langley Research Center Hampton, VA 23665 (804) 864-4960 *Dept. of Engineering University of Denver Denver, CO 80208-0177 (303) 871-2102 Submitted for publication to the Journal of the Acoustical Society of
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm4561.ps.Z, 19950309 NASA Technical Memorandum 4561 Extended Cooperative Control Synthesis John B. Davidson and David K. Schmidt August 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/tp3100.ps.Z, 19950309
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/phd-93-nixon.ps.Z, 19950309
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3418.ps.Z, 19950309 NASA Technical Paper 3418 Design and Evaluation of an Electromagnetic Beam Waveguide for Measuring Electrical Properties of Materials M. C. Bailey February 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/conf-2www-94-nelson-bianco.ps.Z, 19950309 The World Wide Web and Technology Transfer at NASA Langley Research Center1 Michael L. Nelson Systems Analyst, Information Systems Division, NASA Langley Research Center David J. Bianco Systems Analyst, Computer Sciences Corporation, NASA Langley Research Center
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3403.ps.Z, 19950309 NASA Technical Paper 3403 Flight Test of Takeoff Performance Monitoring System David B. Middleton, Raghavachari Srivatsan, and Lee H. Person, Jr. May 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/90/conf-ieee-us-90.ps.Z, 19950309 EFFECT OF STRESS ON ENERGY FLUX DEVIATION OF ULTRASONIC WAVES IN ULTRASONIC WAVES IN GR/EP COMPOSITES William H. Prosser, R. D. Kriz, and Dale W. Fitting* NASA Langley Research Center, Hampton, VA 23681-0001 Virginia Tech, Blacksburg, VA 24061 *NIST, Boulder, CO 80303-3328 Proceedings of the IEEE
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/90/jae-9-4.ps.Z, 19950309 AE Source Orientation by Plate Wave Analysis* Michael R. Gorman Aeronautics and Astronautics Naval Postgraduate School Monterey, CA 93943 William H. Prosser NASA Langley Research Center Hampton, VA 23665 Journal of Acoustic Emission, Vol. 9(4), (1991) pp. 283-288
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4373.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/tp3125.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm108985.ps.Z, 19950309 Contents List of Symbols : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : 5 Introduction : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : :
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/jcm-26-14-92.ps.Z, 19950309 Extensional and Flexural Waves in a Thin-Walled Graphite/Epoxy Tube* William H. Prosser NASA Langley Research Center Hampton, VA 23665 Michael R. Gorman Aeronautics and Astronautics Naval Postgraduate School Monterey, CA 93943 John Dorighi** NASA Langley Research Center Hampton, VA 23665 Journal of
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/jtht-6-4-92.ps.Z, 19950309 Development of a Nonequilibrium Radiative Heating Prediction Method for Coupled Flowfield Solutions Lin C. Hartung NASA Langley Research Center, Hampton, VA 23665-5225
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/89/cr4239.ps.Z, 19950309 Formal Verification of the Interactive Convergence Clock Synchronization Algorithm1 John Rushby and Friedrich von Henke Computer Science Laboratory SRI International Technical Report CSL-89-3R February 1989, Revised August 1991 1This work was performed for the National Aeronautics and Space
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4314.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/conf-rpqnde-93-p1793.ps.Z, 19950309 A PROBABILISTIC MODEL FOR SIMULATING MAGNETOACOUSTIC EMISSION RESPONSES IN FERROMAGNETS J. P. Fulton and B. Wincheski Analytical Services and Materials, Inc. 107 Research Drive Hampton, VA 23666 M. Namkung NASA, Langley Research Center Hampton, VA 23681 INTRODUCTION Magnetoacoustic emission (MAE) is a
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/phd-91-hartung.ps.Z, 19950309 Nonequilibrium Radiative Heating Prediction Method for Aeroassist Flowfields with Coupling to Flowfield Solvers by Lin C. Hartung A Thesis Submitted to the Graduate Faculty of North Carolina State University in Partial Fulfillment of the Requirements for the Degree of Doctor of Philosophy Major Subject:
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/ijcse-4-4-6-41.ps.Z, 19950309 Linear Static Structural and Vibration Analysis on High-Performance Computers Majdi Baddourah and Olaf O. Storaasli and Susan Bostic Computational Mechanics Branch NASA Langley Research Center Hampton, VA 23665-5225 (804)-864-2927
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/90/jrpc-9-2-90.ps.Z, 19950309 Tensile Stress Acoustic Constants of Unidirectional Graphite/Epoxy Composites Journal of Reinforced Plastics and Composites, Vol. 9 (March, 1990) pp. 127-133 W. H. PROSSER NASA Langley Research Center M. S. 231 Hampton, VA 23681-0001 (804) 864-4960 Tensile Stress Acoustic Constants of Unidirectional
	1 See THE LEO PARTICULATE ENVIRONMENT AS DETERMINED BY LDEF Thomas H. See1, Michael E. Zolensky2, Friedrich H rz2, Ronald P. Bernhard1, Kimberly S. Leago1, Jack L. Warren1, Clyde A. Sapp1, Tammy R. Foster1, and William H. Kinard3>ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/conf-space-94-p618.ps.Z 1 See THE LEO PARTICULATE ENVIRONMENT AS DETERMINED BY LDEF Thomas H. See1, Michael E. Zolensky2, Friedrich H rz2, Ronald P. Bernhard1, Kimberly S. Leago1, Jack L. Warren1, Clyde A. Sapp1, Tammy R. Foster1, and William H. Kinard3, 19950309
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3233.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm4549.ps.Z, 19950309 NASA Technical Memorandum 4549 Effect of Passive Venting on Static Pressure Distributions in Cavities at Subsonic and Transonic Speeds Robert L. Stallings, Jr., Elizabeth B. Plentovich, Maureen B. Tracy, and Michael J. Hemsch June 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/aiaa-92-1057.ps.Z, 19950309 - 1 - ELEMENTS OF DESIGNING FOR COST Edwin B. Dean * NASA Langley Research Center Hampton VA Resit Unal ** Old Dominion University Norfolk VA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3261.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4402.ps.Z, 19950309 Summary This paper presents a strategy for dynamically monitoring digital controllers in the laboratory for susceptibility to electromagnetic disturbances that compromise control integrity . The integrity of digital control systems operating in harsh electromagnetic environments can be compromised by
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3461.ps.Z, 19950309 NASA Technical Paper 3461 Natural Frequency of Uniform and Optimized Tetrahedral Truss Platforms K. Chauncey Wu and Mark S. Lake November 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3394.ps.Z, 19950309 NASA Technical Paper 3394 Lifetimes of Lunar Satellite Orbits Kurt W. Meyer, James J. Buglia, and Prasun N. Desai March 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/aiaa-94-4372.ps.Z, 19950309 1 A Distributed Computing Environment for Multidisciplinary Design R. P. Weston* and J. C. Townsend* NASA Langley Research Center, Hampton, VA 23681-0001 T. M. Eidson High Technology Corporation, Hampton, VA 23666 R. L. Gates Computer Sciences Corporation, Hampton, VA 23666 * Research Scientist, AIAA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/aiaa-94-2197.ps.Z, 19950309 1 APPLICATIONS OF AUTOMATIC DIFFERENTIATION IN CFD Alan Carle* Rice University, Houston, Texas Lawrence L. Green NASA Langley Research Center, Hampton, Virginia Christian H. Bischof Argonne National Laboratory, Argonne, Illinois Perry A. Newman NASA Langley Research Center, Hampton, Virginia * Research
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/tp3173.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3240.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3485.ps.Z, 19950309 NASA Technical Paper 3485 Finite Element Method for Eigenvalue Problems in Electromagnetics C. J. Reddy, Manohar D. Deshpande, C. R. Cockrell, and Fred B. Beck December 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3439.ps.Z, 19950309 NASA Technical Paper 3439 Approximate Analysis for Repeated Eigenvalue Problems With Applications to ControlsStructures Integrated Design Sean P. Kenny and Gene J. W. Hou June 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/tm4641.ps.Z, 19950309 NASA Technical Memorandum 4641 Effects of Yaw and Pitch Motion on Model Attitude Measurements Ping Tcheng, John S. Tripp, and Tom D. Finley February 1995 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Memorandum 4641 Effects of Yaw and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/tp3465.ps.Z, 19950309 NASA Technical Paper 3465 ARL Technical Report 518 Integrated Aerodynamic/Dynamic/Structural Optimization of Helicopter Rotor Blades Using Multilevel Decomposition Joanne L. Walsh, Katherine C. Young, Jocelyn I. Pritchard, Howard M. Adelman, and Wayne R. Mantay January 1995
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3452Vol1.ps.Z, 19950309 NASA Technical Paper 3452 Volume 1 HiRel: Hybrid Automated Reliability Predictor (HARP) Integrated Reliability Tool System (Version 7.0) HARP Introduction and User's Guide Salvatore J. Bavuso, Elizabeth Rothmann, Joanne Bechta Dugan, Kishor S. Trivedi, Nitin Mittal, Mark A. Boyd, Robert M. Geist, and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm4521.ps.Z, 19950309 NASA Technical Memorandum 4521 Techniques To Improve Maneuver Stability Characteristics of a Nonlinear Wide-Body Transport Airplane in Cruise Flight William D. Grantham, Lee H. Person, Jr., Melvin L. Bailey, and Stephen A. Tingas March 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/90/iaa-ceso-11-90.ps.Z, 19950309 - 1 - The Design-To-Cost Manifold by Edwin B. Dean NASA Langley Research Center presented at the International Academy of Astronautics Symposium on Space Systems Cost Methodologies and Applications San Diego California U.S.A. May 10-11, 1990
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/aiaa-92-4541.ps.Z, 19950309 1 TRIAL MANEUVER GENERATION AND SELECTION IN THE PALADIN TACTICAL DECISION GENERATION SYSTEM Alan R. Chappell* Lockheed Engineering and Sciences Company Hampton, Virginia Dr. John W. McManus** and Kenneth H. Goodrich NASA Langley Research Center Hampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/rp1334.ps.Z, 19950309 NASA Reference Publication 1334 48-Inch Lidar Aerosol Measurements Taken at the Langley Research Center July 1991 to December 1992 David C. Woods, M. T. Osborn, D. M. Winker, R. J. DeCoursey, and Otto Youngbluth, Jr. July 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm4514.ps.Z, 19950309 NASA Technical Memorandum 4514 Fiber-Optic-Based Laser Vapor Screen Flow Visualization System for Aerodynamic Research in Larger Scale Subsonic and Transonic Wind Tunnels Gary E. Erickson and Andrew S. Inenaga January 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/conf-asnt-94-p226.ps.Z, 19950309 Detection of Fatigue Cracks at Rivets with Self-Nulling Probe Buzz Wincheski, Jim Fulton and Shridhar Nath Analytical Services and Materials 107 Research Drive Hampton, VA 23666 Min Namkung Mail Stop 231 NASA Langley Research Center Hampton, VA 23681-0001 A new eddy current probe developed at NASA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm4506.ps.Z, 19950309 NASA Technical Memorandum 4506 Computational Prediction of Isolated Performance of an Axisymmetric Nozzle at Mach Number 0.90 John R. Carlson February 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/conf-5-tfaw.ps.Z, 19950309 SOME USEFUL INNOVATIONS WITH TRASYS AND SINDA-85 Fifth Annual Thermal and Fluids Analysis Workshop August 16-20, 1993 NASA Lewis Research Center and The Ohio Aerospace Institute Ruth M. Amundsen National Aeronautics and Space Administration Langley Research Center 1 SOME USEFUL INNOVATIONS WITH TRASYS
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4334.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/cp3275-95-ldmdsigjsc.ps.Z, 19950309 LDEF METEOROID & DEBRIS SPECIAL INVESTIGATION GROUP INVESTIGATIONS AND ACTIVITIES AT THE JOHNSON SPACE CENTER Thomas H. See Michael E. Zolensky Ronald P. Bernhard Lockheed Engineering & Science Co. NASA / Johnson Space Center Lockheed Engineering & Science Co. Houston, Texas 77058 Houston, Texas 77058
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/89/aiaa-89-3312.ps.Z, 19950309 DEVELOPMENT OF A TACTICAL GUIDANCE RESEARCH AND EVALUATION SYSTEM (TGRES) Kenneth H. Goodrich*, John W. McManus+ NASA Langley Research Center, Hampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3452Vol4.ps.Z, 19950309 NASA Technical Paper 3452 Volume 4 HiRel: Hybrid Automated Reliability Predictor (HARP) Integrated Reliability Tool System (Version 7.0) HARP Output (HARPO) Graphics Display User s Guide Darrell W. Sproles and Salvatore J. Bavuso November 1994 National Aeronautics and Space Administration Langley
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/conf-tech2001-v1.ps.Z, 19950309 REDUCING THE COMPLEXITY OF THE SOFTWARE DESIGN PROCESS WITH OBJECT-ORIENTED DESIGN M. P. Schuler (804) 864-6732 NASA Langley Research Center Hampton, VA 23665-5225
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/conf-rpqnde-93-p349.ps.Z, 19950309 MUTUAL INDUCTANCE PROBLEM FOR A SYSTEM CONSISTING OF A CURRENT SHEET AND A THIN METAL PLATE J.P. Fulton, B. Wincheski, and S. Nath Analytical Services and Materials, Inc. 107 Research Drive Hampton, VA 23666 M. Namkung NASA Langley Research Center Hampton, VA 23681 INTRODUCTION Rapid inspection of
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/tp3124.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/conf-rpqnde-93-p1785.ps.Z, 19950309 CHARACTERISTICS OF FERROMAGNETIC FLUX FOCUSING LENS IN THE DEVELOPMENT OF SURFACE/SUBSURFACE FLAW DETECTOR Buzz Wincheski, Jim Fulton, and Shridhar Nath Analytical Services and Materials 107 Research Drive Hampton, VA 23666 Min Namkung NASA Langley Research Center MS 231 Hampton, VA 23681 John Simpson
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3409.ps.Z, 19950309 NASA Technical Paper 3409 Time Series Comparisons of Satellite and Rocketsonde Temperatures in 1978{79 Ellis E. Remsberg, Praful P. Bhatt, and Francis J. Schmidlin April 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3237.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/aiaa-94-4261.ps.Z, 19950309 AIAA 94 4261 PARALLEL CALCULATION OF SENSITIVITY DERIVATIVES FOR AIRCRAFT DESIGN USING AUTOMATIC DIFFERENTIATION C. H. Bischof MCS Division, Argonne National Laboratory Argonne, Illinois 60439 L. L. Green, K. J. Haigler MDOB/FMAD, NASA Langley Research Center Hampton, Virginia 23681 0001 T. L. Knauff,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/lpi-94-05.ps.Z, 19950309 LDEF METEOROID AND DEBRIS DATABASE. C.B. Dardano1, T.H. See1, and M.E. Zolensky2, 1Lockheed Engineering & Sciences Co., Houston, Texas 77058, 2NASA - Johnson Space Center, Houston, Texas 77058 The Long Duration Exposure Facility (LDEF) Meteoroid & Debris Special Investigation Group (M&D SIG) database is
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/aiaa-92-3099.ps.Z, 19950309 1 AIAA-92-3099 INTERNAL SHOCK INTERACTIONS IN PROPULSION/AIRFRAME INTEGRATED THREE-DIMENSIONAL SIDEWALL COMPRESSION SCRAMJET INLETS by Scott D. Holland* and John N. Perkins Department of Mechanical and Aerospace Engineering North Carolina State University Raleigh, North Carolina 27695
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm107606.ps.Z, 19950309 A High Angle of Attack Inviscid Shuttle Orbiter Computation William L. Kleb and K. James Weilmuenstery NASA Langley Research Center, Hampton, Virginia, 23665
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4383.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/tm4316.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm4528.ps.Z, 19950309 NASA Technical Memorandum 4528 Experimental and Theoretical Study of Aerodynamic Characteristics of Some Lifting Bodies at Angles of Attack From -10o to 53o at Mach Numbers From 2.30 to 4.62 M. Leroy Spearman and Abel O. Torres March 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/conf-rpqnde-93-p1611.ps.Z, 19950309 AUTOMATED WELD CHARACTERIZATION USING THE THERMOELECTRIC METHOD J. P. Fulton and B. Wincheski Analytical Services and Materials, Inc. 107 Research Drive Hampton, VA 23666 M. Namkung NASA, Langley Research Center Hampton, VA 23681 INTRODUCTION The effective assessment of the integrity of welds is a
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4307.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/conf-10-dasc.ps.Z, 19950309 1 DESIGN AND ANALYSIS TOOLS FOR CONCURRENT BLACKBOARD SYSTEMS John W. McManus Mail Stop 489 NASA Langley Research Center Hampton, Virginia 23665 Summary A blackboard system consists of a set of knowledge sources, a blackboard data structure, and a control strategy used to activate the knowledge sources.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4377.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/cp3194-93-p313.ps.Z, 19950309 CONTINUED INVESTIGATION OF LDEF'S STRUCTURAL FRAME AND THERMAL BLANKETS BY THE METEOROID & DEBRIS SPECIAL INVESTIGATION GROUP Thomas H. See Kimberly S. Mack Jack L. Warren Lockheed Engineering & Science Co. Lockheed Engineering & Science Co. Lockheed Engineering & Science Co. Houston, Texas 77058
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/jtht-6-3-92-carlson.ps.Z, 19950309 DIRECT SIMULATION OF REENTRY FLOWS WITH IONIZATION Ann B. Carlson* NASA Langley Research Center H. A. Hassan** North Carolina State University
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3470.ps.Z, 19950309 NASA Technical Paper 3470 Multiple-Scattering Model for Inclusive Proton Production in Heavy Ion Collisions Francis A. Cucinotta November 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3278.ps.Z, 19950309 NASA Technical Paper 3278 AVSCOM Technical Report 93-A-003 February 1993 Flight Investigation of the Effect of Tail Boom Strakes on Helicopter Directional Control Henry L. Kelley, Cynthia A. Crowell, Kenneth R. Yenni, and Michael B. Lance
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3385.ps.Z, 19950309 NASA Technical Paper 3385 November 1993 Internal Performance of a Nonaxisymmetric Nozzle With a Rotating Upper Flap and a Center-Pivoted Lower Flap David J. Wing, Laurence D. Leavitt, and Richard J. Re
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3264.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3443.ps.Z, 19950309 NASA Technical Paper 3443 Measurements of Unsteady Pressure and Structural Response for an Elastic Supercritical Wing Clinton V. Eckstrom, David A. Seidel, and Maynard C. Sandford November 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm4516.ps.Z, 19950309 NASA Technical Memorandum 4516 Piloted Simulation Study of an ILS Approach of a Twin-Pusher Business/Commuter Turboprop Aircraft Configuration Donald R. Riley, Jay M. Brandon, and Louis J. Glaab January 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/conf-13-ispa-dean.ps.Z, 19950309 Presented May 1991 at the Thirteenth Annual Conference of the International Society of Parametric Analysts - 1 - MODELING PERSONNEL TURNOVER IN THE PARAMETRIC ORGANIZATION by Edwin B. Dean NASA Langley Research Center BACKGROUND A primary issue in organizing a new parametric cost analysis function is to
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/conf-rpqnde-93-p1939.ps.Z, 19950309 NEW EDDY CURRENT PROBE FOR THICKNESS GAUGING OF CONDUCTIVE MATERIALS Buzz Wincheski, Jim Fulton, and Shridhar Nath Analytical Services and Materials 107 Research Drive Hampton, VA 23666 Min Namkung NASA Langley Research Center MS 231 Hampton, VA 23681 INTRODUCTION The accurate measure of material
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3271.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm109141.ps.Z, 19950309 NASA Technical Memorandum 109141 Hypersonic, Nonequilibrium Flow over the FIRE II Forebody at 1634 sec Lin Hartung Chambers Langley Research Center, Hampton, Virginia July 1994 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 1 Hypersonic, Nonequilibrium
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/aiaa-94-0826.ps.Z, 19950309 DIRECT SIMULATION OF EVOLUTION AND CONTROL OF NONLINEAR INSTABILITIES IN ATTACHMENT{LINE BOUNDARY LAYERS Ronald D. Joslin NASA Langley Research Center Hampton, Virginia 23681-0001
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3359.ps.Z, 19950309 NASA Technical Paper 3359 October 1993 Wind-Tunnel Investigation of Aerodynamic Efficiency of Three Planar Elliptical Wings With Curvature of Quarter-Chord Line Raymond E. Mineck and Paul M. H. W. Vijgen
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3194.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3411.ps.Z, 19950309 NASA Technical Paper 3411 Static Performance Investigation of a Skewed-Throat Multiaxis Thrust-Vectoring Nozzle Concept David J. Wing April 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/aiaa-93-1031.ps.Z, 19950309 - 1 - GENOPERSISTATING THE SYSTEM Edwin B. Dean * NASA Langley Research Center Hampton VA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3243.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/conf-rpqnde-93-p1507.ps.Z, 19950309 DISBOND DETECTION IN BONDED ALUMINUM JOINTS USING LAMB WAVE AMPLITUDE AND TIME-OF-FLIGHT Keun J. Sun Department of Physics College of William and Mary Williamsburg, VA 23187 Patrick H. Johnston NASA-Langley Research Center Hampton, VA 23681 INTRODUCTION In recent years, there was a need of developing
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3244.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm4566.ps.Z, 19950309 NASA Technical Memorandum 4566 ATCOM Technical Report 94-A-013 Navier-Stokes and Potential Theory Solutions for a Helicopter Fuselage and Comparison With Experiment Mark S. Chaffin and John D. Berry June 1994
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/cp3143-alter.ps.Z, 19950309 Cell Volume Control at a Surface for Three-Dimensional Grid Generation Packages Stephen J. Alter , Lockheed Engineering & Sciences Company, Hampton, Virginia and Kenneth J. Weilmuenstery NASA Langley Research Center, Hampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tm4363.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/rp1279.ps.Z, 19950309 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/conf-14-ispa.ps.Z, 19950309 - 1 - Dean The Many Dimensions of Program Management presented at the Fourteenth Annual Conference of the International Society of Parametric Analysts Munich Germany 25-27 May 1992 by Edwin B. Dean National Aeronautics and Space Administration Langley Research Center Hampton VA U.S.A. INTRODUCTION For
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm107756.ps.Z, 19950309 LOUDNESS AND ANNOYANCE RESPONSE TO SIMULATED OUTDOOR AND INDOOR SONIC BOOMS by Jack D. Leatherwood and Brenda M. Sullivan SUMMARY The sonic boom simulator of the Langley Research Center was used to quantify subjective loudness and annoyance response to simulated indoor and outdoor sonic boom signatures.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3405.ps.Z, 19950309 NASA Technical Paper 3405 December 1993 Momentum Loss in Proton-Nucleus and Nucleus-Nucleus Collisions Ferdous Khan and Lawrence W. Townsend
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/tp3497.ps.Z, 19950322 NASA Technical Memorandum 3497 Heavy Ion Track-Structure Calculations for Radial Dose in Arbitrary Materials Francis A. Cucinotta, Robert Katz, John W. Wilson, and Rajendra R. Dubey February 1995 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/tm4613.ps.Z, 19950322 NASA Technical Memorandum 4613 Radar Cross-Section Measurements and Simulation of a Tethered Satellite The Small Expendable Deployer System End-Mass Payload Robin L. Cravey, Dion T. Fralick, and Erik Vedeler February 1995 National Aeronautics and Space Administration Langley Research Center Hampton,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/tm4577.ps.Z, 19950322 NASA Technical Memorandum 4577 Acoustic Receptivity Due to Weak Surface Inhomogeneities in Adverse Pressure Gradient Boundary Layers Meelan Choudhari, Lian Ng, and Craig Streett February 1995
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/tp3498.ps.Z, 19950322 NASA Technical Paper 3498 Comparison of Exact Solution With Eikonal Approximation for Elastic Heavy Ion Scattering Rajendra R. Dubey, Govind S. Khandelwal, Francis A. Cucinotta, and Khin Maung Maung February 1995
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/tm4583.ps.Z, 19950322 NASA Technical Memorandum 4583 Wing Pressure Distributions From Subsonic Tests of a High-Wing Transport Model Zachary T. Applin, Garl L. Gentry, Jr., and M. A. Takallu January 1995
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm109172.ps.Z, 19950322 NASA Technical Memorandum 109172 A Strategy for Electronic Dissemination of NASA Langley Technical Publications Donna G. Roper, Mary K. McCaskill, Scott D. Holland, Joanne L. Walsh, Michael L. Nelson, Susan L. Adkins, Manjula Y. Ambur, and Bryan A. Campbell December 1994 National Aeronautics and Space
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/cp3247-p257.ps.Z, 19950420 IMPLEMENTATION OF A DECOUPLED CONTROLLER FOR A MAGNETIC SUSPENSION SYSTEM USING ELECTROMAGNETS MOUNTED IN A PLANAR ARRAY D. E. Cox N. J. Groom NASA Langley Research Center Hampton, VA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/tm110153.ps.Z, 19950420 NASA Technical Memorandum 110153 Integration of Design, Structural, Thermal and Optical Analysis and User s Guide for Structural-to-Optical Translator (PATCOD) R. M. Amundsen, W. S. Feldhaus, A. D. Little, and M. V. Mitchum Langley Research Center, Hampton, Virginia March 1995 National Aeronautics and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/aiaa-91-1496.ps.Z, 19950420 Study of Cluster Formation and its Effects on Rayleigh and Raman Scattering Measurements in a Mach 6 Wind Tunnel by B. Shirinzadeh,* M. E. Hillard,* A. B. Blair, and R. J. Exton* NASA Langley Research Center Hampton, VA 23665
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/jfm-95-p369.ps.Z, 19950420 Direct simulation of evolution and control of three-dimensional instabilities in attachment-line boundary layers By RONALD D. JOSLIN Fluid Mechanics and Acoustics Division, Mail Stop 170 NASA Langley Research Center, Hampton, Virginia 23681-0001, U.S.A. The spatial evolution of three-dimensional
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/jao-92-21-30.ps.Z, 19950420 PLANAR RAYLEIGH SCATTERING RESULTS IN HELIUM/AIR MIXING EXPERIMENTS IN A MACH 6 WIND TUNNEL by B. Shirinzadeh, R. Jeffrey Balla, M. E. Hillard, J. B. Anders, and R. J. Exton NASA Langley Research Center Hampton, VA 23665 and I. A. Waitz California Institute of Technology Pasadena, CA 91125
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/jaiaa-92-30-2.ps.Z, 19950420 Effect of Compliant Walls on Secondary Instabilities in Boundary-Layer Transition Ronald D. Josliny NASA Langley Research Center, Hampton, Virginia 23681 and Philip J. Morrisz Pennsylvania State University, University Park, Pennsylvania 16802
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/conf-asnt-95-p213.ps.Z, 19950420 1995 ASNT Spring Conference and Fourth Annual Research Symposium, pp. 213-215. Las Vegas, Nevada, March 20-24, 1995 (A work of the US Government. Not subject to copyright by ASNT.) Detection and Location of Transverse Matrix Cracks in Cross-Ply Gr/Ep Composites Using Acoustic Emission W. H. Prosser K.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/jaiaa-91-29-2.ps.Z, 19950420 CONDENSATION EFFECTS ON RAYLEIGH SCATTERING MEASUREMENTS IN A SUPERSONIC WIND TUNNEL by B. Shirinzadeh, M. E. Hillard, and R. J. Exton Instrument Research Division, NASA Langley Research Center Hampton, VA 23665
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/jpof-94-6-11.ps.Z, 19950420 Metamorphosis of a Hairpin Vortex into a Young Turbulent Spot Bart A. Singer Research Scientist, High Technology Corp. Mail Stop 156, NASA Langley Research Center Hampton, VA 23681-0001 and Ronald D. Joslin Research Scientist Mail Stop 156, NASA Langley Research Center Hampton, VA 23681-0001 March 17,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/conf-shpcfv-92.ps.Z, 19950420 AUTOMATIC DIFFERENTIATION OF ADVANCED CFD CODES FOR MULTIDISCIPLINARY DESIGN C. Bischof1 and G. Corliss 2 Argonne National Laboratory, Argonne, Illinois L. Green NASA Langley Research Center, Hampton, Virginia A. Griewank1 Argonne National Laboratory, Argonne, Illinois K. Haigler and P. Newman NASA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/cp3247-p583.ps.Z, 19950420 ROBUST TRACKING CONTROL OF A MAGNETICALLY SUSPENDED RIGID BODY Kyong B. Lim and David E. Coxy NASA Langley Research Center Hampton, Virginia SUMMARY This study is an application of H1 and -synthesis for designing robust tracking controllers for the Large Angle Magnetic Suspension Test Facility (LAMSTF).
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/aiaa-95-1825.ps.Z, 19950420 Effects of Sonic Line Transition on Aerothermodynamics of the Mars Pathfinder Probe Peter A. Gnoffo and K. James Weilmuenster and Robert D. Braun and Christopher I. Cruzy NASA Langley Research Center Hampton, VA 23681-0001
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/conf-acc-94-p3198.ps.Z, 19950420 EXPERIMENTAL ROBUST CONTROL STUDIES ON AN UNSTABLE MAGNETIC SUSPENSION SYSTEM Kyong B. Lim and David E. Coxy NASA Langley Research Center Hampton, Virginia Summary This study is an experimental investigation of the robustness of various controllers designed for the Large Angle Magnetic Suspension Test
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/aiaa-95-6093.ps.Z, 19950501 AIAA 95-6093Low-Speed Wind Tunnel Tests of TwoWaverider Configuration ModelsRobert J. PeggDavid E. HahneCharles E. Cockrell, Jr.NASA Langley Research CenterHampton, VA 23681-0001Sixth International Aerospace Planes andHypersonics Technologies ConferenceApril 3-7, 1995 / Chattanooga, TennesseeFor
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/tp3491.ps.Z, 19950501 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3491 Design Tool for Multiprocessor Scheduling and Evaluation of Iterative Dataflow Algorithms Robert L. Jones III Langley Research Center Hampton, Virginia April 1995 Printed copies
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/tp3524.ps.Z, 19950501 NASA Technical Paper 3524 Radiation Safety Aspects of Commercial High-Speed Flight Transportation John W. Wilson, John E. Nealy, Francis A. Cucinotta, Judy L. Shinn, Ferenc Hajnal, Marcel Reginatto, and Paul Goldhagen May 1995
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/tm4610.ps.Z, 19950501 NASA Technical Memorandum 4610 Internal Performance Characteristics of Thrust-Vectored Axisymmetric Ejector Nozzles Milton Lamb March 1995 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Memorandum 4610 Internal Performance
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/tp3516.ps.Z, 19950501 NASA Technical Paper 3516 Airfoil Modification Effects on Subsonic and Transonic Pressure Distributions and Performance for the EA-6B Airplane Dennis O. Allison and William G. Sewall May 1995
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/tp3486.ps.Z, 19950501 NASA Technical Paper 3486 Reduced Dimer Production in Solar-Simulator- Pumped Continuous Wave Iodine Lasers Based on Model Simulations and Scaling and Pumping Studies Robert C. Costen, John H. Heinbockel, Gilda A. Miner, Willard E. Meador, Jr., Bagher M. Tabibi, Ja H. Lee, and Michael D. Williams March
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/conf-iemc-92.ps.Z, 19950501 QUALITY FUNCTION DEPLOYMENT FOR LARGE SYSTEMS Edwin B. Dean MS 325 Space Exploration Initiative Office NASA Langley Research Center Hampton VA 23665
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/aiaa-92-4720.ps.Z, 19950501 INFORMATION MANAGEMENT FOR A LARGE MULTIDISCIPLINARY PROJECT Kennie H. Jones NASA Langley Research Center Hampton, VA 23681 Donald P. Randall NASA Langley Research Center Hampton, VA 23681 Catherine K. Cronin NASA Langley Research Center Hampton, VA 23681
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/tp3494.ps.Z, 19950501 NASA Technical Paper 3494 A Class of Stabilizing Controllers for Flexible Multibody Systems Suresh M. Joshi, Atul G. Kelkar, and Peiman G. Maghami May 1995
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/aiaa-95-1689.ps.Z, 19950504 1 American Institute of Aeronautics and Astronautics A GRID GENERATION SYSTEM FOR MULTI-DISCIPLINARY DESIGN OPTIMIZATION William T. Jones* Jamshid Samareh-Abolhassani Computer Sciences Corporation Hampton, Virginia 23666
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/aiaa-93-2793.ps.Z, 19950509 APPLICATION OF AN ENGINEERING INVISCID-BOUNDARY LAYER METHOD TO SLENDER THREE-DIMENSIONAL VEHICLE FOREBODIES Christopher J. Riley NASA Langley Research Center, Hampton, VA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/aiaa-92-0499.ps.Z, 19950509 AN ENGINEERING AERODYNAMIC HEATING METHOD FOR HYPERSONIC FLOW Christopher J. Riley NASA Langley Research Center, Hampton, VA Fred R. DeJarnettey North Carolina State University, Raleigh, NC
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/phd-92-riley.ps.Z, 19950509 An Engineering Method for Interactive Inviscid-Boundary Layers in Three-Dimensional Hypersonic Flows by Christopher J. Riley A Thesis Submitted to the Graduate Faculty of North Carolina State University in Partial Fulfillment of the Requirements for the Degree of Doctor of Philosophy Major Subject:
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/NASA-adpa-91-p529.ps.Z, 19950511 EXPLORATORY STUDY OF THE ACOUSTIC PERFORMANCE OF PIEZOELECTRIC ACTUATORS O. L. Santa Maria NASA Langley Research Center Hampton, Virginia and E. M. Thurlow, M. G. Jones Lockheed Engineering & Sciences Co. Hampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/NASA-AHS-92.ps.Z, 19950512 Tiltrotor Acoustic Flight Test: Terminal Area Operations By O.L. Santa Maria, Applied Acoustics Branch NASA Langley Research Center Hampton, Virginia and J.B. Wellman, Aeroflightdynamics Directorate NASA Ames Research Center Moffett Field, California and D.A. Conner, Aerostructures Directorate NASA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-ijap-95-tsa.ps.Z, 19950516 THE EVALUATION OF TWO CDU CONCEPTS AND THEIR EFFECTS ON FMS TRAINING Terence S. Abbott NASA - Langley Research Center Hampton, VA 23681-0001
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-ijap-95-mtp.ps.Z, 19950516 1 SUMMARY OF A CREW-CENTERED FLIGHT DECK DESIGN PHILOSOPHY FOR HIGH-SPEED CIVIL TRANSPORT (HSCT) AIRCRAFT Michael T. Palmer, NASA Langley Research Center, Hampton, Virginia William H. Rogers, Bolt, Beranek, & Newman, Inc., Cambridge, Massachusetts Hayes N. Press, Lockheed Engineering & Sciences Company,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tp3496.ps.Z, 19950516 NASA Technical Paper 3496 Numerical Study To Assess Sulfur Hexafluoride as a Medium for Testing Multielement Airfoils Daryl L. Bonhaus and W. Kyle Anderson Langley Research Center Hampton, Virginia Dimitri J. Mavriplis Institute for Computer Applications in Science and Engineering Langley Research
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-aiaa-95-1687.ps.Z, 19950516 Rapid Airplane Parametric Input Design (RAPID) Robert E. Smithy Malcolm I. G. Bloorz Michael J. Wilsonx Almuttil M. Thomas{
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm110160.ps.Z, 19950517 NASA Technical Memorandum 110160 A Finite Element Propagation Model For Extracting Normal Incidence Impedance In Nonprogressive Acoustic Wave Fields Willie R. Watson Langley Research Center, Hampton, Virginia Michael G. Jones Lockheed Engineering & Sciences Company Sharon E. Tanner and Tony L. Parrott
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm109184.ps.Z, 19950531 1 A Study of Workstation Computational Performance for Real-Time Flight Simulation Jeffrey M. Maddalon Jeff I. Cleveland II Summary This paper presents the results of a computational benchmark, based on actual real-time flight simulation code of an X-29 aircraft used at Langley Research Center. This
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-aiaa-95-3414.ps.Z, 19950531 Copyright 1995 by the American Institute of Aeronautics and Astronautics, Inc. No copyright is asserted in the United States under Title 17, U.S. Code. The U.S. Government has a royalty-free license to exercise all rights under the copyright claimed herein for government purposes. All other rights are
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/90/NASA-90-tm102716.ps.Z, 19950601 NASA Technical Memorandum 102716 Formal Design and Verification of a Reliable Computing Platform For Real-Time Control Phase 1 Results Ben L. Di Vito Ricky W. Butler James L. Caldwell October 1990 NASA Langley Research Center Hampton, VA 23665{5225 Contents 1 Introduction 3 2 A Science of Reliable
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-ieee-95-compassrwb.ps.Z, 19950601 NASA Langley's Research and Technology-Transfer Program in Formal Methods Ricky W. Butler James L. Caldwell Victor A. Carre~no C. Michael Holloway Paul S. Miner Assessment Technology Branch NASA Langley Research Center Hampton, Virginia Ben L. Di Vito V GYAN Inc. Hampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-cp3291p689-96.ps.Z, 19950601 MULTILEVEL ELLIPTIC SMOOTHING OF LARGE THREE-DIMENSIONAL GRIDS C. Wayne Mastin Mail Stop 125 NASA Langley Research Center Hampton, VA 23681 SUMMARY Elliptic grid generation methods have been used for many years to smooth and improve grids generated by algebraic interpolation schemes. However, the
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-cr4675.ps.Z, 19950605 NASA Contractor Report 4675 A Verification Procedure for MSC/NASTRAN Finite Element Models Alan E. Stockwell Lockheed Engineering & Sciences Company, Hampton, Virginia Prepared for Langley Research Center Under Contract NAS1-19000 May 1995 i Acknowledgments The author wishes to acknowledge the
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/NASA-qnde-94-p2035.ps.Z, 19950606 APPLICATION OF SELF NULLING EDDY CURRENT PROBE TECHNIQUE TO THE DETECTION OF FATIGUE CRACK INITIATION AND CONTROL OF TEST PROCEDURES S. Nath , M. Namkung, B. Wincheski and J. P. Fulton , NASA Langley Research Center, MS 231 Hampton, VA 23681 Analytical Services and Materials, Inc. 107 Research Dr.,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/NASA-qnde-94-p1577.ps.Z, 19950606 AN ULTRASONIC STUDY ON ANELASTICITY IN METALS J. P. Fulton, S. Nath, and B. Wincheski Analytical Services and Materials, Inc. 107 Research Drive Hampton, VA 23666 M. Namkung Mail Stop 231 NASA, Langley Research Center Hampton, VA 23681 INTRODUCTION Ultrasonic waves are highly sensitive to
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-aiaa-95-1855.ps.Z, 19950606 1 American Institute of Aeronautics and Astronautics APPLICATION OF A NAVIER-STOKES SOLVER TO THE ANALYSIS OF MULTIELEMENT AIRFOILS AND WINGS USING MULTIZONAL GRID TECHNIQUES Kenneth M. Jones* NASA Langley Research Center Hampton, VA Robert T. Biedron Analytical Services and Materials, Inc. Hampton, VA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/NASA-qnde-94-p2317.ps.Z, 19950606 A NEW ELECTROMAGNETIC INSTRUMENT FOR THICKNESS GAUGING OF CONDUCTIVE MATERIALS J. P. Fulton, B. Wincheski, and S. Nath Analytical Services and Materials, Inc. 107 Research Drive Hampton, VA 23666 J. Reilly, and M. Namkung NASA, Langley Research Center Hampton, VA 23681 INTRODUCTION Eddy current
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm109168.ps.Z, 19950607 1 FLUTTER CLEARANCE FLIGHT TESTS OF AN OV-10A AIRPLANE MODIFIED FOR WAKE VORTEX FLIGHT EXPERIMENTS By Robert V. Doggett, Jr.; Jose A. Rivera, Jr.; and Eric C. Stewart NASA Langley Research Center Hampton, VA 23681-0001 SUMMARY Envelope expansion, flight flutter tests of a modified OV-10A aircraft are
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm4640.ps.Z, 19950607 NASA Technical Memorandum 4640 Low-Speed Wind-Tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings With Sweep Angles of 50 Scott P. Fears Lockheed Engineering & Sciences Company Hampton, Virginia Holly M. Ross and Thomas M. Moul Langley Research Center Hampton,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm4603.ps.Z, 19950607 NASA Technical Memorandum 4603 Hydrogen Film Cooling With Incident and Swept-Shock Interactions in a Mach 6.4 Nitrogen Free Stream George C. Olsen and Robert J. Nowak Langley Research Center Hampton, Virginia June 1995 Printed copies available from the following: NASA Center for AeroSpace Information
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm110150.ps.Z, 19950607 Transport Delays Associated with the NASA Langley Flight Simulation Facility by R. Marshall Smith Victoria I. Chung Debbie Martinez Summary This paper describes the transport delays associated with flight simulation programs currently operating at the NASA Langley Research Center (LaRC). Formulas are
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm4695.ps.Z, 19950613 NASA Technical Memorandum 4695 Optimization of Measurements With Pressure Sensitive Paints Donald M. Oglesby Old Dominion University Norfolk, Virginia Chith K. Puram ViGYAN, Inc. Hampton, Virginia Billy T. Upchurch Langley Research Center Hampton, Virginia June 1995 Printed copies available from the
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm110167.ps.Z, 19950613 Defining the IEEE-854 Floating-Point Standard in PVS Paul S. Miner P.S.Miner@LaRC.NASA.Gov Technical Memorandum 110167 NASA Langley Research Center Hampton, VA 23681-0001 June 1995
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm4656.ps.Z, 19950614 NASA Technical Memorandum 4656 Abrasion-Ablation Model for Neutron Production in Heavy Ion Reactions Francis A. Cucinotta, John W. Wilson, and Lawrence W. Townsend June 1995 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Memorandum 4656
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-ses-95-whp.ps.Z, 19950615 Introduction The operation of damage mechanisms in a material or structure under load produces transient acoustic waves. These acoustic waves are known as acoustic emission (AE). In composites they can be caused by a variety of sources including matrix cracking, fiber breakage, and delamination. AE
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tp3502.ps.Z, 19950615 NASA Technical Paper 3502 Experimental Investigation of Inlet-Combustor Isolators for a Dual-Mode Scramjet at a Mach Number of 4 Saied Emami Lockheed Engineering & Sciences Company Hampton, Virginia Carl A. Trexler Langley Research Center Hampton, Virginia Aaron H. Auslender Lockheed Engineering &
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm4658.ps.Z, 19950616 NASA Technical Memorandum 4658 High-Precision Buffer Circuit for Suppression of Regenerative Oscillation John S. Tripp, David A. Hare, and Ping Tcheng Langley Research Center Hampton, Virginia May 1995 Printed copies available from the following: NASA Center for AeroSpace Information National Technical
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tp3495.ps.Z, 19950616 NASA Technical Paper 3495 HZETRN: Description of a Free-Space Ion and Nucleon Transport and Shielding Computer Program John W. Wilson Langley Research Center Hampton, Virginia Francis F. Badavi Christopher Newport University Newport News, Virginia Francis A. Cucinotta and Judy L. Shinn Langley Research
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-cp3291p69-86.ps.Z, 19950619 GEOmetry LABoratory (GEOLAB) Surface Modeling and Grid Generation Technology and Services Patricia A. Kerr Robert E. Smith Mary-Anne K. Posenau 9 May 1995
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-aiaa-95-1835.ps.Z, 19950620 AIAA 95-1835 13th AIAA Applied Aerodynamics Conference June 19 22, 1995 / San Diego, CA EFFICIENCY AND ACCURACY OF TIME-ACCURATE TURBULENT NAVIER-STOKES COMPUTATIONS Christopher L. Rumsey,1,* Mark D. Sanetrik,2,* Robert T. Biedron,2 N. Duane Melson,1, and Edward B. Parlette3 1NASA Langley Research
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm4660.ps.Z, 19950621 NASA Technical Memorandum 4660 Drag Measurements of an Axisymmetric Nacelle Mounted on a Flat Plate at Supersonic Speeds Jeffrey D. Flamm and Floyd J. Wilcox, Jr. Langley Research Center Hampton, Virginia June 1995 Printed copies available from the following: NASA Center for AeroSpace Information
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm4611.ps.Z, 19950623 NASA Technical Memorandum 4611 Measurements of Store Forces and Moments and Cavity Pressures for a Generic Store In and Near a Box Cavity at Subsonic and Transonic Speeds Robert L. Stallings, Jr., E. B. Plentovich, M. B. Tracy, and Michael J. Hemsch May 1995
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tp3518.ps.Z, 19950628 NASA Technical Paper 3518 Structural Analysis and Testing of an Erectable Truss for Precision Segmented Reflector Application Timothy J. Collins, W. B. Fichter, and Richard R. Adams Langley Research Center Hampton, Virginia Mehzad Javeed Lockheed Engineering & Sciences Company Hampton, Virginia July
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm4675.ps.Z, 19950703 NASA Technical Memorandum 4675 Parameterized Spectral Distributions for Meson Production in Proton-Proton Collisions John P. Schneider and John W. Norbury University of Wisconsin La Crosse, Wisconsin Francis A. Cucinotta Langley Research Center Hampton, Virginia June 1995 Printed copies available from
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tp3509.ps.Z, 19950705 NASA Technical Paper 3509 Afterbody/Nozzle Pressure Distributions of a Twin-Tail Twin-Engine Fighter With Axisymmetric Nozzles at Mach Numbers From 0.6 to 1.2 David J. Wing May 1995 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm4652.ps.Z, 19950705 NASA Technical Memorandum 4652 Separation Characteristics of Generic Stores From Lee Side of an Inclined Flat Plate at Mach 6 Floyd J. Wilcox, Jr. May 1995 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Memorandum 4652 Separation
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tp3515.ps.Z, 19950705 NASA Technical Paper 3515 Study of Potential Aerodynamic Benefits From Spanwise Blowing at Wingtip Raymond E. Mineck June 1995 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3515 Study of Potential Aerodynamic Benefits From
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm4639.ps.Z, 19950706 NASA Technical Memorandum 4639 A Ruggedness Evaluation of Procedures for Damage Threshold Testing Optical Materials Matthew W. Hooker, Milfred E. Thomas, Stephanie A. Wise, and Nina D. Tappan February 1995 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm110164.ps.Z, 19950710 NASATechnicalMemorandum 110164 Manual for a Workstation-based Generic Flight Simulation Program (LaRCsim)Version 1.4 E. Bruce Jackson Langley Research Center Hampton, Virginia April 1995 Summary LaRCsim is a set of ANSI C routines that implement a full set of equations of motion for a rigid-body
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm110173.ps.Z, 19950712 TABLE OF CONTENTS Summary .................................................................................................................................... 1 Introduction ................................................................................................................................ 1
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm4664.ps.Z, 19950713 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Memorandum 4664 Computer Model To Simulate Testing at the National Transonic Facility Raymond E. Mineck, Lewis R. Owens, Jr., Richard A. Wahls, and Judith A. Hannon Langley Research Center
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm110172.ps.Z, 19950713 NASA Technical Memorandum 110172 A MANUAL FOR PYROTECHNIC DESIGN, DEVELOPMENT AND QUALIFICATION Laurence J. Bement Langley Research Center, Hampton, Virginia Morry L. Schimmel Schimmel Company, St. Louis, Missouri June 1995 National Aeronautics and Space Administration Langley Research Center Hampton,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm4592.ps.Z, 19950713 NASA Technical Memorandum 4592 ASSIST User Manual Sally C. Johnson Langley Research Center Hampton, Virginia David P. Boerschlein Lockheed Engineering & Sciences Company Hampton, Virginia August 1995 Printed copies available from the following: NASA Center for AeroSpace Information National Technical
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm110174.ps.Z, 19950714 NASA Technical Memorandum 110174 Solution of the Three-Dimensional Helmholtz Equation with Nonlocal Boundary Conditions Steve L. Hodge Virginia Consortium for Engineering and Science, Hampton, Virginia William E. Zorumski and Willie R. Watson Langley Research Center, Hampton, Virginia May 1995 National
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-qfd-95-p27.ps.Z, 19950714 - 1 - PARAMETRIC COST DEPLOYMENT by Edwin B. Dean Senior Research Engineer Multidisciplinary Design Optimization Branch NASA Langley Research Center Hampton, VA 23681 (804) 864-8213 e.b.dean@larc.nasa.gov
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-aiaa-95-2016.ps.Z, 19950718 1 Copyright 1995 by the American Institute of Aeronautics and Astronautics, Inc. No copyright is asserted in the United States under Title 17, U.S. Code. The U.S. Government has a royalty-free license to exercise all rights under the copyright claimed herein for Governmental Purposes. All other rights
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tp3522.ps.Z, 19950719 NASA Technical Paper 3522 A Longitudinal Aerodynamic Data Repeatability Study for a Commercial Transport Model Test in the National Transonic Facility R. A. Wahls and J. B. Adcock Langley Research Center Hampton, Virginia D. P. Witkowski and F. L. Wright Boeing Commercial Airplane Company Seattle,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm4649.ps.Z, 19950728 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Memorandum 4649 Low-Speed Wind-Tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings With Sweep Angles of 60 Thomas M. Moul Langley Research Center
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-ceas-aiaa-95-029.ps.Z, 19950731 A B S T R A C T T h i s p a p e r r e p o r t s o n a n e x p e r i m e n t t o c o n t r o l t h e n o i s e r a d i a t e d f r o m t h e i n l e t o f a d u c t e d f a n u s i n g a t i m e d o m a i n a c t i v e a d a p t i v e s y s t e m . T h e c o n t r o l s o u n d s o u r c e c o n s i s t
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm110147.ps.Z, 19950803 1 Introduction The capability to measure the dielectric properties of various materials has been developed in the Electromagnetic Properties Measurement Laboratory (EPML) of the Electromagnetics Research Branch (ERB). Two measurement techniques which have been implemented in the EPML to characterize
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-cr198197.ps.Z, 19950811 NASA Contractor Report 198197 Analysis of Elliptically Polarized Cavity Backed Antennas Using a Combined FEM/MoM/GTD Technique C. J. Reddy Hampton University, Hampton, Virginia M. D. Deshpande ViGYAN,Inc., Hampton, Virginia D. T. Fralick Lockheed Engineering & Sciences Company, Hampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm4634.ps.Z, 19950814 NASA Technical Memorandum 4634 ATCOM Technical Report 95-A-001 Exploratory Flow Visualization Investigation of Mast-Mounted Sights in Presence of a Rotor Terence A. Ghee and Henry L. Kelley March 1995 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-rp1366.ps.Z, 19950815 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Reference Publication 1366 Cloud Properties Derived From GOES-7 for Spring 1994 ARM Intensive Observing Period Using Version 1.0.0 of ARM Satellite Data Analysis Program Patrick Minnis Langley
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm4671.ps.Z, 19950816 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Memorandum 4671 Low-Speed Wind-Tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings With Sweep Angles of 70 Holly M. Ross Langley Research Center
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tp3528.ps.Z, 19950816 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3528 Cognitive Models of Pilot Categorization and Prioritization of Flight-Deck Information Jon E. Jonsson McDonnell Douglas Aerospace-West Long Beach, California Wendell R. Ricks
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tp3503.ps.Z, 19950818 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3503 Low-Speed Longitudinal Aerodynamic Characteristics Through Poststall for Twenty-One Novel Planform Shapes Gregory M. Gatlin Langley Research Center Hampton, Virginia Brian E.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm110185.ps.Z, 19950821 Convective and Radiative Heating for Vehicle Return from the Moon and Mars Robert B. Greendyke ViGYAN, Inc. Hampton, VA 23666 and Peter A. Gnoffo NASA Langley Research Center Hampton, VA 23681-0001
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm110192.ps.Z, 19950824 NASA Technical Memorandum 110192 Note on Use of Slope Diffraction Coeffi- cients for Aperture antennas on Finite Ground plane C. R. Cockrell F. B. Beck NASA Langley Research Center, Hampton VA August 1995 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-cr198203.ps.Z, 19950824 NASA Contractor Report Application of FEM to Estimate Complex Permittivity of Dielectric Material at Microwave Frequency Using Waveguide Measurements M. D.Deshpande VIGYAN Inc., Hampton, VA C. J. Reddy Hampton University, Hampton, VA. August 1995 1 Contents Symbols 2 Abstract 4 I Introduction 4 II
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tp3521.ps.Z, 19950825 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3521 The NASA Langley 16-Foot Transonic Tunnel Historical Overview, Facility Description, Calibration, Flow Characteristics, and Test Capabilities Francis J. Capone, Linda S. Bangert,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tp3519.ps.Z, 19950828 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3519 PLATSIM: An Efficient Linear Simulation and Analysis Package for Large-Order Flexible Systems Peiman G. Maghami and Sean P. Kenny Langley Research Center Hampton, Virginia Daniel
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-rp1348.ps.Z, 19950829 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Reference Publication 1348 Techniques for Modeling the Reliability of Fault-Tolerant Systems With the Markov State-Space Approach Ricky W. Butler and Sally C. Johnson Langley Research Center Hampton,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-cr198199.ps.Z, 19950830
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-cr198200.ps.Z, 19950830
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-cr4682.ps.Z, 19950905 Formal Verification of an Avionics Microprocessor Mandayam K. Srivas Computer Science Laboratory SRI International Menlo Park CA 94025 USA Steven P. Miller Collins Commercial Avionics Rockwell International Cedar Rapids, IA 52498 USA SRI International Computer Science Laboratory Technical Report
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/NASA-93-thesis-dlb.ps.Z, 19950906 An Upwind Multigrid Method for Solving Viscous Flows on Unstructured Triangular Meshes by Daryl Lawrence Bonhaus B.S. June 1990, University of Cincinnati A Thesis submitted to The Faculty of The School of Engineering and Applied Science of The George Washington University in partial satisfaction of the
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-aiaa-95-1303.ps.Z, 19950906 A SPECTRAL ANALYSIS APPROACH FOR ACOUSTIC RADIATION FROM COMPOSITE PANELS Travis L. Turner NASA Langley Research Center Hampton, VA 23681{0001 Mahendra P. Singhy Virginia Polytechnic Institute and State University Blacksburg, VA 24061{0219 Chuh Meiz Old Dominion University Norfolk, VA 23529{0247
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/NASA-aiaa-94-1324.ps.Z, 19950906 FINITE ELEMENT ANALYSIS OF THE RANDOM RESPONSE SUPPRESSION OF COMPOSITE PANELS AT ELEVATED TEMPERATURES USING SHAPE MEMORY ALLOY FIBERS Travis L. Turnery NASA Langley Research Center Hampton, VA 23681{0001 Z. W. Zhongz and Chuh Mei Old Dominion University Norfolk, VA 23529{0247
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-internoise-95-tlt.ps.Z, 19950906 PREDICTION AND MEASUREMENT OF THE VIBRATION AND ACOUSTIC RADIATION OF PANELS SUBJECTED TO ACOUSTIC LOADING Travis L. Turner and Stephen A. Rizzi Structural Acoustics Branch NASA Langley Research Center Hampton, VA 23681{0001 U.S.A. INTRODUCTION Interior noise and sonic fatigue are important issues in
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-cr4692.ps.Z, 19950907 1 A Guide to the Use of the Pressure Disk Rotor Model as Implemented in INS3D-UP Mark S. Chaffin ViGYAN, Inc. Hampton, Virginia 23666 Summary This is a guide for the use of the pressure disk rotor model that has been placed in the incompressible Navier-Stokes code INS3D-UP. The pressure disk rotor model
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-ssps-95-mgg.ps.Z, 19950907 The Photogrammetric Appendage Structural Dynamics Experiment Dr. Michael G. Gilbert, Sharon S. Welch, & Dr. Christopher L. Moore NASA Langley Research Center Hampton, VA. 23681-0001
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm4648.ps.Z, 19950908 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Memorandum 4648 Mach 10 Experimental Database of a Three-Dimensional Scramjet Inlet Flow Field Scott D. Holland Langley Research Center Hampton, Virginia September 1995 Printed copies
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-ahs-95-dp.ps.Z, 19950912 RESULTS OF AN AEROELASTIC TAILORING STUDY FOR A COMPOSITE TILTROTOR WING David Popelka David Lindsay Group Engineer Rotor Dynamics Principal Engineer Tom Parham, Jr Victor Berry Engineering Specialist Engineering Specialist Bell Helicopter Textron, Inc. Fort Worth, Texas Donald J. Baker Vehicle
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm110182.ps.Z, 19950913 Orbiter Rarefied-Flow Reentry Measurements from the OARE on STS-62 Robert C. Blanchard NASA Langley Research Center Hampton, Virginia 23681-0001 John Y. Nicholson ViGYAN, Inc. Hampton, Virginia 23666-1325
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-internoise-95-kps.ps.Z, 19950915 last name: Shepherd Fig. 4. Coefficient of "log (n)" for Fig. 5. Percent of population "very much" several noise metrics annoyed as a function of sonic boom exposure 1042 interviews were merged with the noise data in order to plot the reactions in each community against noise level. Figure 5 shows that
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm4687.ps.Z, 19950918 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Memorandum 4687 TIA Software User s Manual K. Elliott Cramer Langley Research Center Hampton, Virginia Hazari I. Syed Analytical Services & Materials, Inc. Hampton, Virginia September 1995
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-aiaa-95-2524.ps.Z, 19950918 CALCULATED EFFECTS OF NITRIC OXIDE FLOW CONTAMINATION ON SCRAMJET PERFORMANCE Karen E. Fischer* and Kenneth E. Rock* NASA Langley Research Center, Hampton, VA 23681
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-aiaa-95-2047.ps.Z, 19950918 AIAA 95-2407flAugmented Shock Wave Severanceflof MaterialsLaurence J. BementNASA Langley Research CenterHampton, VA 23681-0001Morry L. SchimmelSchimmel CompanySt. Louis, Missouri31st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and ExhibitSheraton Harbor Island, San Diego, CAflJuly 10 12, 1995flFor
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-asnt-me.ps.Z, 19950922 1 Materials Evaluation, Vol. 53(9), September, 1995, pp. 1052-1058) Advanced, Waveform Based Acoustic Emission Detection of Matrix Cracking in Composites W. H. Prosser, K. E. Jackson , S. Kellas+, B. T. Smith, J. McKeon, and A. Friedman*
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-aiaa-95-3943.ps.Z, 19950925 AIAA 95-3943 Interactive Flutter Analysis and Parametric Study for Conceptual Wing Design Vivek Mukhopadhyay Systems Analysis Branch Aeronautical Systems Analysis Division MS 248, NASA Langley Research Center Hampton, Virginia 23681-0001 1st AIAA Aircraft Engineering, Technology and Operations Congress
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-cr4697.ps.Z, 19951003 Electromagnetic Scattering from a Rectangular Cavity Recessed in a 3D Conducting Surface M. D. Deshpande ViGYAN Inc., Hampton, VA. 23681 C. J. Reddy Hampton University, Hampton, VA. 23666 Contract NAS1-19341 October 1995 National Aeronautics and Space Administration Langley Research Center Hampton,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-cr4691.ps.Z, 19951003 ii TABLE OF CONTENTS ACKNOWLEDGMENTS .......................................................................................................v
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/NASA-ieee-94-icnn.ps.Z, 19951018 A GAMMA MEMORY NEURAL NETWORK FOR SYSTEM IDENTIFICATION Mark A. Motter Jose C. Principe Facility Automated Controls Department of Electrical Engineering NASA Langley Research Center University of Florida Hampton, Virginia 23681 Gainesville, Florida 32611
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-wcnn-95-mam.ps.Z, 19951018 CLASSIFICATION and PREDICTION of WIND TUNNEL MACH NUMBER RESPONSES USING both COMPETITIVE and GAMMA NEURAL NETWORKS Mark A. Motter Jose C. Principe Systems Analysis Branch Department of Electrical Engineering NASA Langley Research Center University of Florida Hampton, Virginia 23681 Gainesville, Florida
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm4694.ps.Z, 19951018 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Memorandum 4694 Reflectometer Distance Measurement Between Parallel Conductive Plates Chase P. Hearn and Robert T. Neece Langley Research Center Hampton, Virginia November 1995 Printed
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-0681.ps.Z, 19951020 AIAA-96-0681Computation of Thermally Perfect CompressibleflFlow Properties34th Aerospace SciencesflMeeting & ExhibitJanuary 15-18, 1996 / Reno, NVFor permission to copy or republish, contact the American Institute of Aeronautics and Astronauticsfl370 L'Enfant Promenade, S.W., Washington, D.C. 20024David
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-ieee-95-tns.ps.Z, 19951020 Effects of Target Fragmentation on Evaluation of LET Spectra From Space Radiation in Low-Earth Orbit (LEO) Environment: Impact on SEU Predictions J. L. Shinn, F. A. Cucinotta, and J. W. Wilson NASA Langley Research Center Hampton, VA 23681-0001 G. D. Badhwar and P. M. O'Neill NASA Johnson Space Center
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm110209.ps.Z, 19951024 1 - NASATM -110209 Recent Improvements in the NASA Technical Report Server Ming-Hokng Maa Michael L. Nelson NASA Langley Research Center October, 1995
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tp3542figs.ps.Z, 19951101 179 L-93-5265 Figure 1. Artist s concept of typical HIDEN nozzle installation. HIDEN nozzles deployedHIDEN nozzle stowed 180 (a) HIDEN nozzle deployed in thrust mode. Figure 2. Typical propulsion integration of HIDEN concept in fan section of HFVT engine. Bearing plane Axis of rotation Fuselage
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tp3542text.ps.Z, 19951101 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3542 Internal Performance of Highly Integrated Deployable Exhaust Nozzles Applicable to Advanced Short-Takeoff and Vertical-Landing Aircraft Scott C. Asbury, Mary L. Mason, and Milton
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-cr198236.ps.Z, 19951101 NASA Contractor Report 198236 User s Manual for CBS3DS Version 1.0 C. J. Reddy Hampton University, Hampton, Virginia M. D. Deshpande ViGYAN,Inc., Hampton, Virginia Contract NAS1-19935 October 1995 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 1
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-ijap-95-mr.ps.Z, 19951101 Published in: (1995) Proceedings of the Eighth International Symposium on Aviation Psychology. Columbus, OH: The Ohio State University Press. (In press) 1 LINE PILOTS' ATTITUDES ABOUT AND EXPERIENCE WITH FLIGHT DECK AUTOMATION: RESULTS OF AN INTERNATIONAL SURVEY AND PROPOSED GUIDELINES Dr. Marianne
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tp3542tbls.ps.Z, 19951101 16 Table 1. Coordinates Defining Internal Flow Path and Turning Vane Geometry of 1.8 CR D-Shaped Nozzles (a) Nozzle internal flow path Spline 1 Spline 2 Spline 3 Spline 4 X, in. Y, in. Z, in. X, in. Y, in. Z, in. X, in. Y, in. Z, in. X, in. Y, in. Z, in. -2.472 1.748 .000 -2.403 1.699 .500 -2.164 1.530
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-0825.ps.Z, 19951102 AIAA 96-0825 Aerodynamic Characteristics of an Aerospace Vehicle During a Subsonic Pitch-Over Maneuver William L. Kleb NASA Langley Research Center Hampton, Virginia Aerodynamic Characteristics of an Aerospace Vehicle During a Subsonic Pitch-Over Maneuver William L. Kleb NASA Langley Research Center,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm110210.ps.Z, 19951103 NASA Technical Memorandum 110210 Aerospace Applications of Integer and Combinatorial Optimization S. L. Padula Langley Research Center, Hampton, Virginia R. K. Kincaid College of William and Mary, Williamsburg, Virginia October 1995 National Aeronautics and Space Administration Langley Research Center
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-0105.ps.Z, 19951106
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/tp3088.ps.Z, 19951113 Contents Tables and Figures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . iv Acronyms . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . v 1. Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 2. Design Processes . . . . . . . . . . . . . . . .
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm110189.ps.Z, 19951128 1 Interpretation of IEEE-854 Floating-Point Standard and Definition in the HOL system Victor A. Carre o NASA Langley Research Center Hampton, VA 23681-0001 v.a.carreno@larc.nasa.gov The ANSI/IEEE Standard 854-1987 for floating-point arithmetic is interpreted by converting the lexical descriptions in the
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-aiaaj-v33n8rdj.ps.Z, 19951201 Active Control of Boundary-Layer Instabilities Part II: Use of Sensors and Spectral Controller R. D. Joslin,1 R. A. Nicolaides,2 G. Erlebacher,3 M.Y. Hussaini,3 and M. D. Gunzburger4 NASA Langley Research Center, Hampton, VA 23681-0001 Introduction This second study focuses on the suppression of
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-aiaaj-v33n7rdj.ps.Z, 19951201 Evolution of Stationary Crossflow Vortices in Boundary Layers on Swept Wings Ronald D. Josliny NASA Langley Research Center
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-aiaa-95-2314.ps.Z, 19951204 26th AIAA Fluid Dynamics Conference June 19-22, 1995/San Diego, CA For permission to copy or republish, contact the American Institute of Aeronautics and Astronautics 370 L'Enfant Promenade, S.W., Washington, D.C. 20024A IAA 95-2314H ypervelocity Aeroheating Measurementsi n Wake of Mars Mission Entry
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-cr198177.ps.Z, 19951208 Fracture Testing of 2324-T39 Aluminum Alloy D. S. Dawicke Analytical Services and Materials, Inc.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm110205.ps.Z, 19951211
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-pf-95-v7n12rdj.ps.Z, 19951212 Growth Characteristics Downstream of a Shallow Bump: Computation and Experiment Ronald D. Joslin NASA Langley Research Center, Hampton, Virginia 23681-0001 and Chester E. Groschy Old Dominion University, Norfolk, Virginia 23529
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm4697.ps.Z, 19951212 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Memorandum 4697 Control Effectiveness and Tip-Fin Dihedral Effects for the HL-20 Lifting-Body Configuration at Mach Numbers From 1.6 to 4.5 Christopher I. Cruz and George M. Ware Langley
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-jsc-95-v10n2rdj.ps.Z, 19951213 Scalability of Parallel Spatial Direct Numerical Simulations on Intel Hypercube and IBM SP1 and SP2 Ronald D. Joslin (Corresponding Author) Flow Modeling and Control Branch NASA Langley Research Center Mail Stop 170 Hampton, VA 23681 (804) 864-2234 Fax: (804) 864-7897 Ulf R. Hanebutte Reactor Analysis
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-cr198248.ps.Z, 19951218 NASA Contractor Report 198248 F-18 High Alpha Research Vehicle (HARV) Parameter Identification Flight Test Maneuvers for Optimal Input Design Validation and Lateral Control Effectiveness E.A. Morelli Lockheed Martin Engineering and Sciences Co. NASA Langley Research Center Hampton, Virginia Contract
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm4701.ps.Z, 19960110 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Memorandum 4701 Buckling Analysis of Debonded Sandwich Panel Under Compression David W. Sleight and John T. Wang Langley Research Center Hampton, Virginia December 1995 Printed copies
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tp3533-figs.ps.Z, 19960110 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3533 NUCFRG2: An Evaluation of the Semiempirical Nuclear Fragmentation Database J. W. Wilson Langley Research Center Hampton, Virginia R. K. Tripathi University of Southern Illinois
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-cr198194.ps.Z, 19960118 PROPERTIES OF A CENTER/SURROUND RETINEX PART ONE: SIGNAL PROCESSING DESIGN Zia-ur Rahman Science and Technology Corporation 101 Research Drive, Hampton, VA 23666
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm110188.ps.Z, 19960118 PROPERTIES OF A CENTER/SURROUND RETINEX PART TWO: SURROUND DESIGN Daniel J. Jobson Glenn A. Woodell NASA Langley Research Center
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tp3533.ps.Z, 19960123
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-0316.ps.Z, 19960129 Aerothermodynamic Analysis of Commercial Experiment Transporter (COMET) Reentry Capsule William A. Wood, Peter A. Gnoffoy and Didier F. G. Raultz NASA Langley Research Center, Hampton, VA 23681 An aerothermodynamic analysis of the Commercial Experiment Transporter (COMET) reentry capsule has been
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm110222.ps.Z, 19960130 COMPUTATIONAL CONSIDERATIONS FOR THE SIMULATION OF SHOCK-INDUCED SOUND Jay Casper Old Dominion University Norfolk, Virginia Mark H. Carpenter NASA Langley Research Center Hampton, Virginia NASA Langley Research Center Technical Memorandum 110222 December, 1995 COMPUTATIONAL CONSIDERATIONS FOR THE
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/NASA-94-tm109057.ps.Z, 19960201 1 The Analysis of a Generic Air-to-Air Missile Simulation Model Joseph A. Kaplan Department of Computer Science Virginia Polytechnic Institute and State University Blacksburg, Virginia Alan R. Chappell Lockheed Engineering and Sciences Corporation Hampton, Virginia John W. McManus Analysis and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110215.ps.Z, 19960207 Christian M. Fernholz The George Washington University Joint Institute for Advancement of Flight Sciences Hampton, VA 23681{0001 Jay H. Robinson NASA Langley Research Center Structural Acoustics Branch Hampton, VA 23681{0001 MSC/NASTRAN's performance in the solution of fully-coupled fluid/structure
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-cr198276.ps.Z, 19960208
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-0877.ps.Z, 19960208 1 SOUND TRANSMISSION THROUGH A CYLINDRICAL SANDWICH SHELL WITH HONEYCOMB CORE Yvette Y. Tang* National Research Council MS 463, NASA Langley Research Center, Hampton, VA 23681 Jay H. Robinson and Richard J. Silcox Structural Acoustic Branch MS 463, NASA Langley Research Center, Hampton, VA 23681
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4702.ps.Z, 19960209 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Memorandum 4702 Airline Transport Pilot Preferences for Predictive Information Anna C. Trujillo Langley Research Center Hampton, Virginia February 1996 Printed copies available from the
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-0903.ps.Z, 19960209 Six Degree-of-Freedom Entry Dispersion Analysis for the METEOR Recovery Module Prasun N. Desai* Robert D. Braun* Richard W. Powell** Walter C. Engelund* Paul V. Tartabini* NASA Langley Research Center Hampton, VA 23681-0001 Aerospace Engineer, Space Systems and Concepts Division, Member AIAA *Senior
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-ijhsc-95-p547.ps.Z, 19960213 A Parallel Prefix Algorithm for Almost Toeplitz Tridiagonal Systems Xian-He Sun Ronald D. Joslin Dept. of Computer Science Mail Stop 170 Louisiana State University NASA Langley Research Center Baton Rouge, LA 70803-4020 Hampton, VA 23681-0001
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-fme-96-bld.ps.Z, 19960215 Formalizing New Navigation Requirements for NASA's Space Shuttle Ben L. Di Vito V GYAN, Inc., 30 Research Drive, Hampton, Virginia 23666, USA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-0711.ps.Z, 19960220 1 American Institute of Aeronautics and Astronautics MULTIDISCIPLINARY AEROSPACE DESIGN OPTIMIZATION: SURVEY OF RECENT DEVELOPMENTS Jaroslaw Sobieszczanski-Sobieski* NASA Langley Research Center Hampton, Virginia 23681 (j.sobieski@larc.nasa.gov) Raphael T. Haftka University of Florida Gainesville,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-0151.ps.Z, 19960220 AN EFFICIENT AND ROBUST METHOD FOR PREDICTING HELICOPTER ROTOR HIGH-SPEED IMPULSIVE NOISE Kenneth S. Brentner NASA Langley Research Center Hampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-cr4713.ps.Z, 19960222 NASA Contractor Report 4713 Robust Stabilization of Uncertain Systems Based on Energy Dissipation Concepts Sandeep Gupta Vigyan, Inc. Hampton, VA 23666 Prepared for Langley Research Center under Grant NAS1-19341 March 1996
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aas-96-189.ps.Z, 19960222 AAS 96-189 ON-ORBIT APPLICATION OF H-INFINITY TO THE MIDDECK ACTIVE CONTROLS EXPERIMENT: OVERVIEW OF RESULTS Jessica A. Woods-Vedeler* and Lucas G. Horta The Middeck Active Control Experiment (MACE) was successfully completed during the flight of STS-67 in March 1995. MACE provided an on-orbit
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-cr198288.ps.Z, 19960229 NASA Contractor Report 198288 Constrained Solution of a System of Matrix Equations Sandeep Gupta Vigyan, Inc. Hampton, VA 23666 Prepared for Langley Research Center under Grant NAS1 19341 February 1996
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-rp1376vol2.ps.Z, 19960308 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Reference Publication 1376 Volume II Clouds and the Earth s Radiant Energy System (CERES) Algorithm Theoretical Basis Document Volume II Geolocation, Calibration, and ERBE-Like Analyses (Subsystems 1
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-rp1376vol3.ps.Z, 19960308 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Reference Publication 1376 Volume III Clouds and the Earth s Radiant Energy System (CERES) Algorithm Theoretical Basis Document Volume III Cloud Analyses and Determination of Improved Top of
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-rp1376vol1.ps.Z, 19960311 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Reference Publication 1376 Volume I Clouds and the Earth s Radiant Energy System (CERES) Algorithm Theoretical Basis Document Volume I Overviews (Subsystem 0) CERES Science Team Langley Research
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-rp1376vol4.ps.Z, 19960312 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Reference Publication 1376 Volume IV Clouds and the Earth s Radiant Energy System (CERES) Algorithm Theoretical Basis Document Volume IV Determination of Surface and Atmosphere Fluxes and Temporally
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-adh.soc-96-jgs.ps.Z, 19960313 CHEMISTRY AND PROPERTIES OF IMIDE OLIGOMERS CONTAINING PENDANT AND TERMINAL PHENYLETHYNYL GROUPS Joseph G. Smith Jr. NASA Langley Research Center Composites and Polymers Branch Hampton, Virginia 23681-0001 Introduction As part of a continuing effort to develop high performance/high temperature
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/90/NASA-90-tm102614.ps.Z, 19960318 A Parallel-Vector Algorithm for Rapid Structural Analysis on High-Performance Computers Olaf O. Storaasli Structural Mechanics Division NASA Langley Research Center, Hampton, VA 23665-5225 Duc T. Nguyen and Tarun K. Agarwal Department of Civil Engineering Old Dominion University, Norfolk, VA 23529-0369
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-assl-ccj.ps.Z, 19960327 HIGH ENERGY DIODE SIDE-PUMPED Cr:LiSAF LASER Christyl C. Johnson, Donald J. Reichle, Norman P. Barnes NASA Langley Research Center Hampton, VA 23681 Gregory J. Quarles Lightning Optical Corporation Tarpon Springs, FL 34689 James W. Early and Nigel J. Cockroft Los Alamos National Laboratory,MS E535 Los
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tp3475.ps.Z, 19960328 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3475 Analysis of Fluctuating Static Pressure Measurements in the National Transonic Facility William B. Igoe Langley Research Center Hampton, Virginia March 1996 Printed copies
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm110224.ps.Z, 19960415 PHYSICAL AGING EFFECTS ON THE COMPRESSIVE LINEAR VISCOELASTIC CREEP OF IM7/K3B COMPOSITE by David R. Veazie and Thomas S. Gates Langley Research Center, Hampton, Virginia 1
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4674.ps.Z, 19960416 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Memorandum 4674 User s Manual for the Langley Aerothermodynamic Upwind Relaxation Algorithm (LAURA) F. McNeil Cheatwood ViGYAN, Inc. Hampton, Virginia Peter A. Gnoffo Langley Research Center
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-thermo.kec.ps.Z, 19960416 Thermal characterization of defects in aircraft structures via spatially controlled heat application K. Elliott Cramer and William P. Winfree NASA - Langley Research Center 3 E. Taylor St. - MS 231 Hampton, VA 23681-0001
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-das-drj.ps.Z, 19960422 FLIGHT DEMONSTRATION OF INTEGRATED AIRPORT SURFACE AUTOMATION CONCEPTS Denise R. Jones and Steven D. Young NASA Langley Research Center Mail Stop 152D Hampton, VA 23681
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110247.ps.Z, 19960423 NASA TM-110247 INTEGRATING A GENETIC ALGORITHM INTO A KNOWLEDGE-BASED SYSTEM FOR ORDERING COMPLEX DESIGN PROCESSES James L. Rogers NASA Langley Research Center Hampton Virginia Collin M. McCulley Christina L. Bloebaum State University of New York at Buffalo Buffalo, New York April 1996 National
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tp3573.ps.Z, 19960423 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3573 Computational Methods for Frictional Contact With Applications to the Space Shuttle Orbiter Nose-Gear Tire Comparisons of Experimental Measurements and Analytical Predictions John
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110241.ps.Z, 19960423 TABLE OF CONTENTS 1. Introduction .............................................................................3 2. Background .............................................................................4 2.1 Program Function Overview ..................................4 2.1.1 File Structure
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-1367.ps.Z, 19960423 American Institute of Aeronautics and Astronautics 1 EVALUATION OF THIN KEVLAR-EPOXY FABRIC PANELS SUBJECTED TO SHEAR LOADING Donald J. Baker * Vehicle Structures Directorate - ARL NASA Langley Research Center Hampton, VA 23681 * Aerospace Engineer, Structural Mechanics Branch. Copyright by American
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tp3510.ps.Z, 19960425 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3510 Aeroservoelastic Simulation of an Active Flexible Wing Wind Tunnel Model Carey S. Buttrill, Barton J. Bacon, Jennifer Heeg, and Jacob A. Houck Langley Research Center Hampton,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110256.ps.Z, 19960430 1 A Comprehensive and Cost-Effective Computer Infrastructure for K-12 Schools Gary P. Warren and Jeffrey M. Seaton A White Paper from NASA Langley Research Center s HPCC/IITA K-12 Program 1.0 Introduction The integration of computers and telecommunications into primary and secondary education has become
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-1812.ps.Z, 19960503 C.P. Center of Pressure, m D drag, N DAC DSMC Analysis Code DSMC Direct Simulation Monte Carlo L vehicle reference length, m L/D lift-to-drag ratio n number density, molecules/m3 NURBS Non-Uniform Rational B-Spline P pressure, N/m2 q heat transfer, W/m2 RLV Reusable Launch Vehicle SSTO
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-icngg5.cwm.ps.Z, 19960503 1 Arc Length Based Grid Distribution For Surface and Volume Grids C. Wayne Mastin Mail Stop 125 NASA Langley Research Center Hampton, VA 23681 USA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-cr198269.ps.Z, 19960503 NASA Contractor Report 198269 Parameter Identification Flight Test Maneuvers for Closed Loop Modeling of the F-18 High Alpha Research Vehicle (HARV) E.A. Morelli Lockheed Martin Engineering and Sciences Co. Hampton, Virginia Contract NAS1-19000 May 1996 National Aeronautics and Space Administration
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-cr198268.ps.Z, 19960503 NASA Contractor Report 198268 Piloted Parameter Identification Flight Test Maneuvers for Closed Loop Modeling of the F-18 High Alpha Research Vehicle (HARV) E.A. Morelli Lockheed Martin Engineering and Sciences Co. Hampton, Virginia Contract NAS1-19000 May 1996 National Aeronautics and Space
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-cr198270.ps.Z, 19960503 NASA Contractor Report 198270 Flight Test Maneuvers for Closed Loop Lateral-Directional Modeling of the F-18 High Alpha Research Vehicle (HARV) using Forebody Strakes E.A. Morelli Lockheed Martin Engineering and Sciences Co. Hampton, Virginia Contract NAS1-19000 May 1996 National Aeronautics and Space
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-1706.ps.Z, 19960510 For permission to copy or republish, contact the American Institute of Aeronautics and Astronautics 370 L'Enfant Promenade, S.W., Washington, D.C. 20024 AIAA 96-1706 Numerical Algorithms for Acoustic Integrals{ the Devil is in the Details Kenneth S. Brentner NASA Langley Research Center Hampton,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-ahs_forum.ksb.ps.Z, 19960510 A COMPARISON OF COMPUTATIONAL AEROACOUSTIC PREDICTION METHODS FOR TRANSONIC ROTOR NOISE Kenneth S. Brentner NASA Langley Research Center, Mail Stop 128 Hampton, VA 23681 Anastasios S. Lyrintzisy and Evangelos K. Koutsavdisz School of Aeronautics and Astronautics Purdue University, West Lafayette, IN
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-1762.ps.Z, 19960510 RESPONSE OF A PANEL STRUCTURE FORCED BY THE NOISE FROM A NEARLY SONIC JET C. C. Fenno, Jr. National Research Council, Hampton, VA 23681-0001 A. Bayliss y Northwestern University, Evanston, IL 60208 L. Maestrello z NASA Langley Research Center, Hampton, VA 23681-0001
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110246.ps.Z, 19960514 Prediction of Airfoil Characteristics With Higher Order Turbulence Models Thomas B. Gatski Aerodynamic and Acoustic Methods Branch NASA Langley Research Center, Hampton, VA 23681-0001, USA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-cpne.xhs.ps.Z, 19960516 Performance Comparison of a Set of Periodic and Non-Periodic Tridiagonal Solvers on SP2 and Paragon Parallel Computers Xian-He Sun Stuti Moitra Department of Computer Science Scientific Applications Branch Louisiana State University NASA Langley Research Center Baton Rouge, LA 70803-4020 Hampton, VA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/NASA-92-sre.jmv.ps.Z, 19960520 Improving the Software Development Process Using Testability Research Jeffrey M. Voas Keith W. Miller Reliable Software Technologies Corp. Department of Computer Science Penthouse Suite 101 Jones Hall 1001 North Highland Blvd. College of William & Mary Arlington, VA 22201 Williamsburg, VA 23185
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/NASA-92-sqj.jmv.ps.Z, 19960520 A Dynamic Testing Complexity Metric Jeffrey Voasy Mail Stop 478 NASA-Langley Research Center Hampton, VA 23665
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/NASA-92-iasted.jmv.ps.Z, 19960520 A Model for Assessing the Liability of Seemingly Correct Software Jeffrey M. Voas Larry K. Voasy Keith W. Millerz
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/91/NASA-91-ieeesw.jmv.ps.Z, 19960520 Using Dynamic Sensitivity Analysis to Assess Testability Jeffrey Voas , Larry Morelly, Keith Millerz
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/NASA-92-ieeeswe.jmv.ps.Z, 19960520 PIE: A Dynamic Failure-Based Technique Jeffrey M. Voas, Member, IEEE
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/NASA-92-aqsdt.jmv.ps.Z, 19960520 PISCES: A Tool for Predicting Software Testability Jeffrey M. Voas Keith W. Miller Jeffery E. Payne Room 108 Dept. of Computer Science Room 108 1121 Arlington Blvd. 101 Jones Hall 1121 Arlington Blvd. RST Corp. College of William & Mary RST Corp. Arlington, VA 22209 Williamsburg, VA 23185 Arlington VA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4710.ps.Z, 19960522 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Memorandum 4710 ATCOM Technical Report 96-A-005 Wind Tunnel Test Results of a 1/8-Scale Fan-in-Wing Model John C. Wilson Joint Research Program Office, Aeroflightdynamics Directorate U.S.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm109041.ps.Z, 19960523 Dynamic Stability Instrumentation System (DSIS) Volume II: Operation Software Manual Taumi S. Daniels and Thomas L. Jordan NASA Langley Research Center Hampton, VA 23681 NASA TM-109041 April 1996 1 Table of Contents
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-agardfdp.dah.ps.Z, 19960528 23-1 Presented at the AGARD 78th Fluid Dynamics Panel Meeting and Symposium on The Characterisation & Modification of Wakes from Lifting Vehicles in Fluids, Trondheim, Norway, 20-23 May 1996 An Aircraft Vortex Spacing System (AVOSS) For Dynamical Wake Vortex Spacing Criteria D.A. Hinton NASA, Langley
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-1760.ps.Z, 19960528 1 SOUND TRANSMISSION THROUGH CYLINDRICAL SHELL STRUCTURES EXCITED BY BOUNDARY LAYER PRESSURE FLUCTUATIONS Yvette Y. Tang1 National Research Council MS 463, NASA Langley Research Center, Hampton, VA 23681 Richard J. Silcox2 and Jay H. Robinson3 Structural Acoustical Branch MS 463, NASA Langley Research
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110218.ps.Z, 19960610 NASA Technical Memorandum 110218 An Evaluation of the Measurement Requirements for an In-Situ Wake Vortex Detection SystemHenri D. Fuhrmann and Eric C. Stewart Langley Research Center, Hampton, Virginia May 1996National Aeronautics andSpace AdministrationLangley Research CenterHampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110239.ps.Z, 19960610 ON-ORBIT APPLICATION OF H-INFINITY TO THE MIDDECK ACTIVE CONTROLS EXPERIMENT: OVERVIEW OF RESULTS Jessica A. Woods-Vedeler* and Lucas G. Horta The Middeck Active Control Experiment (MACE) was successfully completed during the flight of STS-67 in March 1995. MACE provided an on-orbit validation of modern
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110260.ps.Z, 19960610 A Viscoelastic Higher-Order Beam Finite Element A. R. Johnson and A. Tessler Computational Structures Branch NASA Langley Research Center, MS 240 Hampton, VA 23681-0001
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-1500.ps.Z, 19960611 American Institute of Aeronautics and Astronautics 1 A Revolute Joint With Linear Load-Displacement Response for Precision Deployable Structures Mark S. Lake* NASA Langley Research Center, Hampton, Virginia, 23681 Peter A. Warren , and Lee D. Peterson University of Colorado, Boulder, Colorado, 80309
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-2496.ps.Z, 19960611 Numerical Simulation of Wake Vortices Measured During the Idaho Falls and Memphis Field Programs Fred H. Proctor NASA Langley Research Center Flight Dynamics & Control Division Hampton, VA 23681-0001 14th AIAA Applied Aerodynamic Conference 17-20 June 1996, New Orleans, Louisiana AIAA Paper No. 96-2496
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-1722.ps.Z, 19960612 BBBBBBBBBBBBBBBBBBBBBBBBBBBBBBBBBBBBBBBBBBBBBBBBBBBB Supervisor, Aeroacoustics and Structural Acoustics Associate Fellow &RSULJKW <=ooss E ) : URVYHOG 3XEOLVKHG E WKH $PHULFDQ ,QVWLWXWH RI $HURQDXWLFV DQG $VWURQDXWLFVffl ,QF ZLWK SHUPLVVLRQ NUMERICAL COMPARISON OF ACTIVE ACOUSTIC AND STRUCTURAL
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tp3587.ps.Z, 19960613 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3587 Buckling and Postbuckling Behavior of Laminated Composite Plates With a Cutout Michael P. Nemeth Langley Research Center Hampton, Virginia July 1996 Printed copies available from
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-2197.ps.Z, 19960617 For permission to copy or republish, contact the American Institute of Aeronautics and Astronautics 370 L Enfant Promenade, S.W., Washington, D.C. 20024 AIAA 96-2197 Calibration of the Langley 8-Foot High Temperature Tunnel for Hypersonic Airbreathing Propulsion Testing Lawrence D. Huebner, Kenneth E.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tp3575.ps.Z, 19960618 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3575 Electromagnetic Scattering Analysis of Arbitrarily Shaped Material Cylinder by FEM-BEM Method M. D. Deshpande VIGYAN, Inc. Hampton, Virginia C. R. Cockrell and C. J. Reddy Langley
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110262.ps.Z, 19960619 Multigrid Approach to Incompressible Viscous Cavity Flows William A. Wood, NASA Langley Research Center, Hampton, VA 23681 Two-dimensional incompressible viscous driven-cavity flows are computed for Reynolds numbers on the range 100{20,000 using a loosely coupled, implicit, second-order
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-1800.ps.Z, 19960621 Analytic Corrections to CFD Heating Predictions Accounting for Changes in Surface Catalysis Peter A. Gnoffo NASA Langley Research Center Hampton, Virginia 23681-0001 and George R. Ingery Iowa State University Ames, Iowa 50011-3231
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-2412.ps.Z, 19960625 AIAA 96-2412flDevelopment of Semi-Span Model flTest TechniquesflWilliam E. Milholen II and Ndaona ChokaniflNorth Carolina State UniversityflRaleigh, NCflRobert J. McGheeflNASA Langley Research CenterflHampton, VA14th AIAA Applied Aerodynamics ConferenceflJune 17 20, 1996 / New Orleans, LAFor permission
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-2416.ps.Z, 19960626 Geometric Model for a Parametric Study of the Blended-Wing-Body Airplane C. Wayne Mastiny Robert E. Smithz Ideen Sadrehaghighix Michael R. Wiese{
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/88-Prior/conf-tims-orsa-denver.ps.Z, 19960626 1 Dynamic Eigenvalue/Eigenvector Tracking Using Continuous Optimization on Constraint Manifolds Edwin B. Dean NASA Langley Research Center Mail Stop 430 Hampton, VA 23665 (804) 865-4894 Presented at the The TIMS/ORSA Joint National Meeting Denver Colorado October 24-26, 1988
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/88-Prior/conf-8-ispa.ps.Z, 19960626 Presented at the 1986 Annual Conference of the International Society of Parametric Analysts - 1 - Cost Risk Analysis Based on Perception of the Engineering Process Edwin B. Dean and Darrell A. Wood NASA Langley Research Center Mail Stop 444 Hampton VA 23665 (804) 865 4894 Arlene A. Moore and Edward H.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/88-Prior/conf-10-ispa.ps.Z, 19960626 1 Linear Least Squares for Correlated Data Edwin B. Dean NASA Langley Research Center Mail Stop 430 Hampton VA 23665 804 865 4894 Presented at the Tenth Annual International Conference of the International Society of Parametric Analysts July 25-27, 1988 Brighton, England Introduction Throughout the
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/88-Prior/cr4187.ps.Z, 19960626 136 Bibliography Jeannette M. Wing. A study of 12 specifications of the library problem. IEEE Software, 5(4):666, July 1988. Patrick Henry Winston. Artificial Intelligence. Addison-Wesley, Reading, Massachusetts, second edition, 1984. David D. Woods. Cognitive technologies: The
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/88-Prior/conf-9-ispa.ps.Z, 19960626 Proceedings of the Ninth Annual Conference of The International Society of Parametric Analysts, San Diego CA, May 5-7, 1987 - 1 - Using the MCPLXS Generator for Technology Transfer Arlene A. Moore PRC Kentron International Inc. 3221 W. Armistead Ave. Hampton VA 23665 Edwin B. Dean NASA Langley Research
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/88-Prior/conf-tims-orsa.ps.Z, 19960626 1 Continuous Optimization on Constraint Manifolds by Edwin B. Dean NASA Langley Research Center Presented at the TIMS/ORSA Joint National Meeting Washington D.C. April 25-27, 1988
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tp3569.ps.Z, 19960628 1 2 3 4 5 Summary A bistatic k-space image concept for frequency domain (FD) electromagnetic (EM) computer codes is presented. The concept enables images to be computed without the frequency sweep required for experimental images, which results in a significant reduction in computational effort. This
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110254.ps.Z, 19960701 NASA Technical Memorandum 110254 On Longitudinal Control of High Speed Aircraft in the Presence of Aeroelastic Modes Suresh M. Joshi NASA Langley Research Center, Hampton, Virginia Atul G. Kelkar Kansas State University, Manhattan, Kansas May 1996 National Aeronautics and Space Administration Langley
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tp3579.ps.Z, 19960712 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3579 Assessment of Dual-Point Drag Reduction for an Executive-Jet Modified Airfoil Section Dennis O. Allison and Raymond E. Mineck Langley Research Center Hampton, Virginia July 1996
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tp3559.ps.Z, 19960715 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3559 Aerodynamic Characteristics of Two Waverider-Derived Hypersonic Cruise Configurations Charles E. Cockrell, Jr. and Lawrence D. Huebner Langley Research Center Hampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110252.ps.Z, 19960716
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-2502.ps.Z, 19960716 For permission to copy or republish, contact the American Institute of Aeronautics and Astronautics370 L'Enfant Promenade, S.W., Washington, D.C. 20024AIAA 96-2502A Method for the Constrained Design ofNatural Laminar Flow AirfoilsBradford E. Green and John L. WhitesidesThe George Washington
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm110165.ps.Z, 19960716 NASA Technical Memorandum 110165Analytical Comparison of Three StiffenedPanel ConceptsJill M. Maloney and K. Chauncey WuLangley Research Center, Hampton, VirginiaJames C. RobinsonAnalytical Services & Materials, Inc., Hampton, VirginiaDecember 1995National Aeronautics andSpace AdministrationLangley
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-0782.ps.Z, 19960716 This paper is declared a work of the US Government and is not subject to copyright protection in the United States.HYPERSONIC BOUNDARY LAYER STABILITY OVER A FLARED CONE IN A QUIET TUNNELJason T. Lachowicz* and Ndaona Chokani North Carolina State University, Raleigh NC 27695andStephen P. Wilkinson NASA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4726.ps.Z, 19960717 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Memorandum 4726 Subsonic Aerodynamic Characteristics of a Circular Body Earth-to-Orbit Vehicle Roger A. Lepsch, Jr. and George M. Ware Langley Research Center Hampton, Virginia Ian O.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-4018.ps.Z, 19960717 USE OF THE COLLABORATIVE OPTIMIZATION ARCHITECTURE FOR LAUNCH VEHICLE DESIGN R.D. Braun A.A. Moorey Space Systems and Concepts Division NASA Langley Research Center Hampton, Virginia 23681 I.M. Krooz Dept. of Aeronautics and Astronautics Stanford University Stanford, CA 94305
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-2544.ps.Z, 19960717 HIGHREYNO LDS N UMBER ANALYSIS OFFLATPLATEANDSEP ARATEDAFTERBODYFLOWUSING NON-LINEAR TURBULENCE MODELSJ ohnR. Carlson NASALangleyResearchCenterHampton, VAA bstractTheabilityofthethree-dimensionalNavier-Stokesmethod, PAB3D,tosimulatethe effectofReynolds num-b er variationusing non-linear
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-iciam.rdb.ps.Z, 19960717 Development and Application of the Collaborative Optimization Architecture in a Multidisciplinary Design Environment R. D. Braun I. M. Krooy August 14, 1995
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110216.ps.Z, 19960722 iSUMMARYThis report and a previous report, NASA TM 107601, "Simulation Model of a Twin-Tail,High Performance Airplane," (ref. 1.0), document the aircraft model and computer programwhich form the nonlinear, six degree-of-freedom, batch simulation of the High Alpha ResearchVehicle (HARV), a highly
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-1999.ps.Z, 19960722 AIAA 96-1999 Elliptic Volume Grid Generation for Viscous CFD Parametric Design Studies Stephen J. Alter Lockheed Martin Engineering and Sciences Hampton, Virginia Dr. F. McNeil Cheatwood ViGYAN, Inc. Hampton, Virginia ELLIPTIC VOLUME GRID GENERATION FOR VISCOUS CFD PARAMETRIC DESIGN STUDIES Stephen J.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4714.ps.Z, 19960723 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Memorandum 4714 Artificial Boundary Conditions for Computation of Oscillating External Flows S. V. Tsynkov Langley Research Center Hampton, Virginia August 1996 Printed copies available from
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tp3574.ps.Z, 19960723 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-0001NASA Technical Paper 3574Computational Methods for Frictional ContactWith Applications to the Space Shuttle OrbiterNose-Gear TireDevelopment of Frictional Contact AlgorithmJohn A. TannerLangley Research
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tp3585.ps.Z, 19960723 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3585 A Fast Parallel Tridiagonal Algorithm for a Class of CFD Applications Xian-He Sun Louisiana State University Baton Rouge, Louisiana Stuti Moitra Langley Research Center Hampton,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tp3557.ps.Z, 19960723 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-0001NASA Technical Paper 3557Improved Method for Prediction of AttainableWing Leading-Edge ThrustHarry W. CarlsonLockheed Engineering & Sciences Company Hampton, VirginiaMarcus O. McElroy and Wendy B.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4707.ps.Z, 19960723 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-0001NASA Technical Memorandum 4707A Method for Characterizing ThermosetPolyimidesC. Ranganathaiah, D. R. Sprinkle, and R. H. PaterLangley Research Center Hampton, VirginiaA. EftekhariHampton University Hampton,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tp3584.ps.Z, 19960723 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3584 ATCOM TR-96-A-007 Wake Geometry Measurements and Analytical Calculations on a Small-Scale Rotor Model Terence A. Ghee Analytical Services & Materials, Inc. Hampton, Virginia John
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tp3552.ps.Z, 19960723 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-0001NASA Technical Paper 3552Closed-Form Evaluation of Mutual Coupling ina Planar Array of Circular AperturesM. C. BaileyLangley Research Center Hampton, VirginiaApril 1996 Printed copies available from the
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tp3572.ps.Z, 19960723 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-0001NASA Technical Paper 3572On-Line Measurement of Heat of Combustionof Gaseous Hydrocarbon Fuel MixturesDanny R. SprinkleLangley Research Center Hampton, VirginiaSushil K. Chaturvedi and Ali KheireddineOld
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tp3591.ps.Z, 19960723 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-0001NASA Technical Paper 3591Effect of Full-Chord Porosity on AerodynamicCharacteristics of the NACA0012 AirfoilRaymond E. MineckLangley Research Center Hampton, VirginiaPeter M. HartwichViGYAN Inc. Hampton,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4672.ps.Z, 19960723 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-0001NASA Technical Memorandum 4672Dataflow Design ToolUser s ManualRobert L. Jones IIILangley Research Center Hampton, VirginiaFebruary 1996 Printed copies available from the following:NASA Center for AeroSpace
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-0301.ps.Z, 19960724 For permission to copy or republish, contact the American Institute of Astronautics and Aeronautics370 L'Enfant Promenade, S.W. Washington, D.C. 2002434th Aerospace SciencesMeeting and ExhibitJanuary 15-18, 1996 / Reno, NevadaAIAA 96-0301Observation of Vibrational Relaxation Dynamicsin X3 g Oxygen
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tp3561.ps.Z, 19960724 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-0001NASA Technical Paper 3561Managing Approach Plate Information Study(MAPLIST): An Information RequirementsAnalysis of Approach Chart UseWendell R. RicksLangley Research Center Hampton, VirginiaJon E.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-2754.ps.Z, 19960726 1American Institute of Aeronautics and AstronauticsFUNCTIONAL PERFORMANCE OF PYROVALVESLaurence J. Bement*NASA Langley Research CenterHampton, VAAbstractFollowing several flight and ground test failures ofspacecraft systems using single-shot, "normally closed"pyrotechnically actuated valves
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110252.errata.ps.Z, 19960726 1 Wilkie, W. Keats, and Park, K. C.,"An Aeroelastic Analysis of Helicopter Rotor Blades Incorporating Piezoelectric Fiber Composite Twist Actuation," NASA TM 110252, U.S. Army Research Laboratory Report 328, May 1996. ERRATA (compiled as of 7/23/96) p.5: (clarification) Although not stated, small angles
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tp3603.ps.Z, 19960729 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3603 Technique for Extension of Small Antenna Array Mutual-Coupling Data to Larger Antenna Arrays M. C. Bailey Langley Research Center Hampton, Virginia August 1996 Printed copies
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110271.ps.Z, 19960729 Page 1 (Re)inventing Government-Industry R&D Collaboration Bruce J. Holmes Introduction Reinventing government has spawned some unexpected surprises. In the NASA Aeronautics Advanced Subsonic Technology Program (AST), new enterprise charters and government business instruments enabled capabilities to
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-2386.ps.Z, 19960729 AIAA 96-2386flStudy of Semi-Span Model TestingflTechniquesG. M. Gatlin and R. J. McGheeflNASA Langley Research CenterflHampton, VA 23681-000114th Applied Aerodynamics ConferenceflJune 17-20, 1996 / New Orleans, LAFor permission to copy or republish, contact the American Institute of Aeronautics and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-fedc.rdj.ps.Z, 19960729 A METHODOLOGY FOR THE AUTOMATED OPTIMAL CONTROL OF FLOWS INCLUDING TRANSITIONAL FLOWS Ronald D. Joslin Max D. Gunzburger Roy A. Nicolaides NASA Langley Research Center Iowa State University Carnegie Mellon University Hampton, VA 23681 Ames, IA 50011 Pittsburgh, PA 15213 Gordon Erlebacher M. Yousuff
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4645vol1appC.ps.Z, 19960729 1Appendix CExperimental Surface Pressure Data for 65 Delta Wing,M =0.85The experimental surface pressure data for the 65 delta wing at constantM =0.85 are summarized in tables C1 C3. Because of the extensive data contained in these tables, they have not been included in the printed copy of the paperbut
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4645vol1.ps.Z, 19960729 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-0001NASA Technical Memorandum 4645Experimental Surface Pressure Data Obtainedon 65 Delta Wing Across Reynolds Numberand Mach Number RangesVolume 1 Sharp Leading EdgeJulio Chu and James M. LuckringLangley
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4645vol1appD.ps.Z, 19960729 1Appendix DExperimental Surface Pressure Data for 65 Delta Wing,Rmac=6 106The experimental surface pressure data for the 65 delta wing at constant Rmac=6 106 are summarized intablesD1 D6. Because of the extensive data contained in these tables, they have not been included in the printed copyof the paper
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-1752.ps.Z, 19960730 AIAA 96-1752 2nd AIAA/CEAS Aeroacoustics Conference May 6 8, 1996 / State College, PA 1 American Institute of Aeronautics and Astronautics COMPUTATION OF ACOUSTIC WAVES THROUGH SLIDING-ZONE INTERFACES USING AN EULER/NAVIER-STOKES CODE Christopher L. Rumsey* NASA Langley Research Center, Mail Stop 128,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-1867.ps.Z, 19960730 31st AIAA Thermophysics Conference June 18-20, 1996 / New Orleans, LA For permission to copy or republish, contact the American Institute of Aeronautics and Astronautics 370 L'Enfant Promenade, S.W., Washington, D.C. 20024A IAA 96-1867C omparison of Experimental andC omputational AerothermodynamicsN
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-cr4709.ps.Z, 19960730 NASA Contractor Report 4709ComputationalAnalysisofSemi-SpanMo delTestTechniquesWilliam E. Milholen, IINdaona ChokaniNorth Carolina State UniversityRaleigh, NCCOOPERATIVE AGREEMENT NCC1-169March 1996 AbstractA computational inv estigation was conducted to support the development of asemi-span model test
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-2240.ps.Z, 19960731 19th AIAA Advanced Measurement and Ground Testing Technology Conference June 18-20, 1996/New Orleans, LA For permission to copy or republish, contact the American Institute of Aeronautics and Astronautics 370 L'Enfant Promenade, S.W., Washington, D.C. 20024A IAA 96-2240H ypervelocity Heat-TransferM
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4645vol2appE.ps.Z, 19960801 1Appendix EExperimental Surface Pressure Data for 65 Delta Wing,Rmac=60 106The experimental surface pressure data for the 65 delta wing at constantRmac=60 106 are summarized intablesE1 E6. Because of the extensive data contained in these tables, they have not been included in the printed copy ofthe
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4645vol2appC.ps.Z, 19960801 1Appendix CExperimental Surface Pressure Data for 65 Delta Wing,M =0.85The experimental surface pressure data for the 65 delta wing at constantM =0.85 are summarized in tables C1 C7. Because of the extensive data contained in these tables, they have not been included in the printed copy of the paperbut
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4645vol2.ps.Z, 19960801 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-0001NASA Technical Memorandum 4645Experimental Surface Pressure Data Obtainedon 65 Delta Wing Across Reynolds Numberand Mach Number RangesVolume 2 Small-Radius Leading EdgeJulio Chu and James M. LuckringLangley
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4645vol2appD.ps.Z, 19960801 1Appendix DExperimental Surface Pressure Data for 65 Delta Wing,Rmac=6 106The experimental surface pressure data for the 65 delta wing at constantRmac=6 106 are summarized intablesD1 D6. Because of the extensive data contained in these tables, they have not been included in the printed copyof the paper
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110265.ps.Z, 19960802 ARTIFICIAL BOUNDARY CONDITIONS BASED ON THE DIFFERENCE POTENTIALS METHOD SEMYON V. TSYNKOVy
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-ilrc-rec.ps.Z, 19960805 Feasibility Study For A Spaceborne Ozone/Aerosol Lidar System Richard E. Campbell1, Edward V. Browell1, Syed Ismail1, Alexander E. Dudelzak2, Allan I. Carswell3, and Arkady Ulitsky4 1 - NASA Langley Research Center, Hampton, Virginia, USA E-mail: r.e.campbell, e.v.browell, or s.ismail@larc.nasa.gov 2 -
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4645vol3appG.ps.Z, 19960807 1Appendix GExperimental Surface Pressure Data for 65 Delta Wing,Rmac=60 106The experimental surface pressure data for the 65 delta wing at constantRmac=60 106 are summarized intablesG1 G4. Because of the extensive data contained in these tables, they have not been included in the printed copyof the
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4645vol4appE.ps.Z, 19960807 1Appendix EExperimental Surface Pressure Data for 65 Delta Wing,Rmac=60 106The experimental surface pressure data for the 65 delta wing at constantRmac=60 106 are summarized intablesE1 E6. Because of the extensive data contained in these tables, they have not been included in the printed copy ofthe
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4645vol3.ps.Z, 19960807 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-0001NASA Technical Memorandum 4645Experimental Surface Pressure Data Obtainedon 65 Delta Wing Across Reynolds Numberand Mach Number RangesVolume 3 Medium-Radius Leading EdgeJulio Chu and James M. LuckringLangley
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4645vol3appE.ps.Z, 19960807 1Appendix EExperimental Surface Pressure Data for 65 Delta Wing,M =0.85The experimental surface pressure data for the 65 delta wing at constantM =0.85 are summarized in tables E1 E11. Because of the extensive data contained in these tables, they have not been included in the printed copy of the paperbut
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4645vol4appD.ps.Z, 19960807 1Appendix DExperimental Surface Pressure Data for 65 Delta Wing,Rmac=6 106The experimental surface pressure data for the 65 delta wing at constantRmac=6 106 are summarized intablesD1 D6. Because of the extensive data contained in these tables, they have not been included in the printed copyof the paper
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4645vol3appC.ps.Z, 19960807 1Appendix CExperimental Surface Pressure Data for 65 Delta Wing,M =0.40The experimental surface pressure data for the 65 delta wing at constantM =0.40 are summarized in tables C1 C3. Because of the extensive data contained in these tables, they have not been included in the printed copy of the paperbut
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4645vol3appF.ps.Z, 19960807 1Appendix FExperimental Surface Pressure Data for 65 Delta Wing,Rmac=6 106The experimental surface pressure data for the 65 delta wing at constantRmac=6 106 are summarized intablesF1 F4. Because of the extensive data contained in these tables, they have not been included in the printed copyofthe paper
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4645vol3appD.ps.Z, 19960807 1Appendix DExperimental Surface Pressure Data for 65 Delta Wing,M =0.60The experimental surface pressure data for the 65 delta wing at constantM =0.60 are summarized in tables D1 D3. Because of the extensive data contained in these tables, they have not been included in the printed copy of the paperbut
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4645vol4.ps.Z, 19960807 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-0001NASA Technical Memorandum 4645Experimental Surface Pressure Data Obtainedon 65 Delta Wing Across Reynolds Numberand Mach Number RangesVolume 4 Large-Radius Leading EdgeJulio Chu and James M. LuckringLangley
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4645vol4appC.ps.Z, 19960807 1Appendix CExperimental Surface Pressure Data for 65 Delta Wing,M =0.85The experimental surface pressure data for the 65 delta wing at constantM =0.85 are summarized in tables C1 C11. Because of the extensive data contained in these tables, they have not been included in the printed copy of thepaper but
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4645vol3appH.ps.Z, 19960807 1Appendix HExperimental Surface Pressure Data for 65 Delta Wing,Rmac=120 106The experimental surface pressure data for the 65 delta wing at constantRmac=120 106 are summarized intablesH1 H4. Because of the extensive data contained in these tables, they have not been included in the printed copyof the
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-cr4749.ps.Z, 19960807 Computation of Thermally Perfect Propertiesof Oblique Shock WavesKenneth E. TatumLockheed Martin Engineering & Sciencesl Hampton, VirginiaNASA Contractor Report 4749National Aeronautics and Space AdministrationLangley Research Centerl Hampton, Virginia 23681-0001August 1996 Computation of Thermally
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-cr4747.ps.Z, 19960808 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-0001NASA Contractor Report 4747Database of Mechanical Properties of TextileCompositesJerry DelbreyLockheed Martin Aeronautical Systems Marietta, GeorgiaAugust 1996Prepared for Langley Research Centerunder
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tp3568.ps.Z, 19960809 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-0001NASA Technical Paper 3568Buckling Behavior of Long Anisotropic PlatesSubjected to Combined LoadsMichael P. NemethLangley Research Center Hampton, VirginiaNovember 1995 Printed copies available from the
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tp3525.ps.Z, 19960809 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-0001NASA Technical Paper 3525Investigation of Piloting Aids for ManualControl of Hypersonic ManeuversDavid L. Raney, Michael R. Phillips, and Lee H. Person, Jr.Langley Research Center Hampton, VirginiaOctober
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tp3544.ps.Z, 19960809 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-0001NASA Technical Paper 3544Electromagnetic Scattering Analysis of aThree-Dimensional-Cavity-Backed Apertureinan Infinite Ground Plane Using a CombinedFinite Element Method/Method of MomentsApproachC. J.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tp3531.ps.Z, 19960809 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-0001NASA Technical Paper 3531Multiaxis Thrust-Vectoring Characteristics of aModel Representative of the F-18 High-AlphaResearch Vehicle at Angles of Attack From 0 to70 Scott C. Asbury and Francis J.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tp3548.ps.Z, 19960809 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-0001NASA Technical Paper 3548Analysis of Three-Dimensional-Cavity-BackedAperture Antennas Using a Combined FiniteElement Method/Method of Moments/Geometrical Theory of Diffraction TechniqueC. J. ReddyLangley
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-cr4752.ps.Z, 19960812 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-0001NASA Contractor Report 4752Using Formal Methods to Assist in theRequirements Analysis of the Space ShuttleGPS Change RequestBen L. Di VitoViGYAN Inc. Hampton, VirginiaLarry W. RobertsLockheed Martin Space
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-4017.ps.Z, 19960813 y z x y z x i ij i i ij c F g s x x y z
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-3860.ps.Z, 19960816 A New Approach to Aircraft Robust Performance Analysis Irene M. Gregory Dynamics and Controls Branch NASA Langley Research Center Hampton, VA Jorge E. Tierno Science and Research Center Honeywell Minneapolis, MN
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tp3570.ps.Z, 19960816 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3570 Performance Assessment of the Digital Array Scanned Interferometer (DASI) Concept Stephen J. Katzberg Langley Research Center Hampton, Virginia Richard B. Statham Lockheed Martin
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-ilrc-asm.ps.Z, 19960819 Development of the Lidar Atmospheric Sensing Experiment (LASE) - An Advanced Airborne DIAL Instrument Alvah S. Moore, Jr., Kevin E. Brown, William M. Hall, James C. Barnes, William C. Edwards, Larry B. Petway1, Alan D. Little, William S. Luck, Jr., Irby W. Jones, Charles W. Antill, Jr., Edward V.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-3991.ps.Z, 19960820 AIAA-96-3991 USE OF CAD GEOMETRY IN MDO Jamshid A. Samareh j.a.samareh@larc.nasa.gov Computer Sciences Corporation, Geometry Laboratory (GEOLAB, http://geolab5.larc.nasa.gov) (ftp://techreports.larc.nasa.gov/pub/techreports/larc/96) 6th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-cr201592.ps.Z, 19960826 NASA Contractor Report 201592 CLMNANAL: A C++ Program for Application of the Coleman Stability Analysis to Rotorcraft Michael B. Lance Lockheed Martin Engineering & Sciences Company Hampton, Virginia Contract NAS1-19000 August 1996 National Aeronautics and Space Administration Langley Research Center
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4719.ps.Z, 19960830 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Memorandum 4719 Static Internal Performance of a Two- Dimensional Convergent-Divergent Nozzle With External Shelf Milton Lamb and John G. Taylor Langley Research Center Hampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-cas-mln.ps.Z, 19960909 THE WORKSTATION CLUSTERING ENVIRONMENT AT NASA LANGLEY RESEARCH CENTER Michael L. Nelson NASA Langley Research Center MS 157A, Hampton VA 23681 (757) 864-8511 m.l.nelson@larc.nasa.gov David E. Cordner NASA Langley Research Center MS 157A, Hampton VA 23681 (757) 864-7325 d.e.cordner@larc.nasa.gov Summary
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tp3596.ps.Z, 19960911 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3596 Numerical Simulation of Jet Aerodynamics Using the Three-Dimensional Navier-Stokes Code PAB3D S. Paul Pao Langley Research Center Hampton, Virginia Khaled S. Abdol-Hamid
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-4157.ps.Z, 19960911 American Institute of Aeronautics and Astronautics 1 DeMAID/GA AN ENHANCED DESIGN MANAGER S AID FOR INTELLIGENT DECOMPOSITION J. L. Rogers* NASA Langley Research Center
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/NASA-aiaa-92-4809.ps.Z, 19960911 1 ENHANCEMENTS TO THE DESIGN MANAGER'S AIDE FOR INTELLIGENT DECOMPOSITION (DeMAID)* James L. Rogers** and Jean-Francois M. Barthelemy+ Interdisciplinary Research Office NASA Langley Research Center Hampton, VA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/NASA-aiaa-94-4326.ps.Z, 19960911 ORDERING DESIGN TASKS BASED ON COUPLING STRENGTHS J. L. Rogers NASA Langley Research Center Hampton, Virginia 23681 C. L. Bloebaum Department of Mechanical and Aerospace Engineering State University of New York at Buffalo Buffalo, New York 14260 AIAA Paper No. 94-4326 to be presented at the Fifth
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-cr4751.ps.Z, 19960912 L O C K H E E D M A R T I N Engineering & Sciences Company NASA Contractors Report 4751 Standard Test Methods for Textile Composites John E. Masters & Marc A. Portanova Lockheed Martin Engineering & Sciences Company, Hampton, Virginia Contract NAS1-19000 September 1996 2 Table of Contents
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-sae-aiaa-96-wac-67.ps.Z, 19960912 Paper No. WAC-67 Structural Concepts Study of Non-circular Fuselage Configurations Vivek Mukhopadhyay Systems Analysis Branch Aeronautical Systems Analysis Division MS 248, NASA Langley Research Center Hampton, Virginia 23681-0001 SAE/AIAA World Aviation Congress October 22-24, 1996 Los Angeles,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-4028.ps.Z, 19960913 1 MDO TEST SUITE AT NASA LANGLEY RESEARCH CENTER Sharon L. Padula, Natalia Alexandrov and Lawrence L. Green NASA Langley Research Center Hampton, VA Sixth AIAA/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization AIAA Paper No. 96-4028 Bellevue, Washington September 4-6, 1996 2 MDO TEST
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110276.ps.Z, 19960913 NASA Technical Memorandum 110276 An Interactive Software for Conceptual Wing Flutter Analysis and Parametric Study Vivek Mukhopadhyay Langley Research Center, Hampton, Virginia August 1996 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 1 AN INTERACTIVE
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110277.ps.Z, 19960917 NASA Technical Memorandum 110277 U. S. Army Research Laboratory Technical Report 1212 Design and Evaluation of a Bolted Joint for a Discrete Carbon-Epoxy Rod-Reinforced Hat Section Donald J. Baker Vehicle Structures Directorate U.S. Army Research Laboratory Langley Research Center, Hampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110278.ps.Z, 19960918 NASA Technical Memorandum 110278 U. S. Army Research Laboratory Technical Report 1213 Analysis of Thick Sandwich Shells With Embedded Ceramic Tiles Carlos G. Davila Vehicle Structures Directorate U.S. Army Research Laboratory Langley Research Center, Hampton, Virginia C. Smith and F. Lumban-Tobing
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-icas-pda.ps.Z, 19960918 20th CongressInternational Council of the Aeronautical SciencesPaper Number 96-5.7.1Airborne Systems Technology Application to theWindshear ThreatP. Douglas Arbuckle,Michael S. Lewis,andDavid A. HintonNASA Langley Research CenterHampton, VAUSASeptember 8-13, 1996SORRENTO, ITALY 1AIRBORNE SYSTEMS
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110275.ps.Z, 19960919 NASA Technical Memorandum 110275 Evaluation of Alternatives for Trichlorotrifluoroethane (CFC-113) to Clean and Verify Liquid Oxygen Systems Michelle L. Morris Langley Research Center, Hampton, Virginia September 1996 National Aeronautics and Space Administration Langley Research Center Hampton,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tp3619.ps.Z, 19960919 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3619 Investigation of Oxygen-Induced Quenching of Phosphorescence in Photoexcited Aromatic Molecules by Positron Annihilation Spectroscopy Jag J. Singh Langley Research Center Hampton,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4736.ps.Z, 19960927 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Memorandum 4736 Acoustic Survey of a 3/8-Scale Automotive Wind Tunnel Earl R. Booth, Jr. Langley Research Center Hampton, Virginia Gary Romberg Chrysler Technology Center Auburn Hills,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tp3617.ps.Z, 19960927 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3617 Microstructural Characterization of Semi-Interpenetrating Polymer Networks by Positron Lifetime Spectroscopy Jag J. Singh and Ruth H. Pater Langley Research Center Hampton,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/97/NASA-97-9car-lhc.ps.Z, 19961002 ____________________________________________*Corresponding author address: Lin H. Chambers,Atmospheric Sciences Division, Mail Stop 420, NASALangley Research Center, Hampton, Virginia 23681-0001; e-mail . COMPUTATION OF THE EFFECTS OF INHOMOGENEOUS CLOUDSON RETRIEVAL OF
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/NASA-97-9car-lhc.ps.Z, 19961002 ____________________________________________*Corresponding author address: Lin H. Chambers,Atmospheric Sciences Division, Mail Stop 420, NASALangley Research Center, Hampton, Virginia 23681-0001; e-mail . COMPUTATION OF THE EFFECTS OF INHOMOGENEOUS CLOUDSON RETRIEVAL OF
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tp3592.ps.Z, 19961003 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3592 Comparison of Turbulence Models for Nozzle-Afterbody Flows With Propulsive Jets William B. Compton III Langley Research Center Hampton, Virginia September 1996 Printed copies
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-cr201593.ps.Z, 19961003 ROTONET Primer Devon Prichard Lockheed Engineering & Sciences Co. Hampton, Virginia 1 October, 1996 ROTONET Primer i TABLE OF CONTENTS TABLE OF CONTENTS i 1 INTRODUCTION 1-1 2 ACOUSTICS REVIEW 2-1 2.1 Concepts : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : : 2-1 2.2 Units : : :
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-40hfes-pcs.ps.Z, 19961004 FLIGHT CREW TASK MANAGEMENT IN NON-NORMAL SITUATIONS Paul C. Schutte Anna C. Trujillo Langley Research Center National Aeronautics and Space Administration Hampton, Virginia Task management (TM) is always performed on the flight deck, although not always explicitly, consistently, or rigorously. Nowhere
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/NASA-97-9car-dpk.ps.Z, 19961007 8.2 THE USE OF CORRELATED k-DISTRIBUTIONS TO ACCOUNT FOR THE RADIATIVE EFFECT OF MOLECULAR ABSORPTION UPON SATELLITE MEASURED RADIANCES David P. Kratz NASA Langley Research Center, Hampton, Virginia 1. INTRODUCTION Establishing the radiative effect of molecular absorption (emission) in the atmosphere is
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/97/NASA-97-9car-dpk.ps.Z, 19961007 8.2 THE USE OF CORRELATED k-DISTRIBUTIONS TO ACCOUNT FOR THE RADIATIVE EFFECT OF MOLECULAR ABSORPTION UPON SATELLITE MEASURED RADIANCES David P. Kratz NASA Langley Research Center, Hampton, Virginia 1. INTRODUCTION Establishing the radiative effect of molecular absorption (emission) in the atmosphere is
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/NASA-93-tm4453.ps.Z, 19961007 NASATechnicalMemorandum4453X-15/HL-20OperationsSupportComparisonW.DouglasMorrisJUNE1993 NASATechnicalMemorandum4453X-15/HL-20OperationsSupportComparisonW.DouglasMorrisLangleyResearchCenterHampton,Virginia AcknowledgmentsThisreportbringstogetherideasandinformationfromseveralindividualswithout
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4727.ps.Z, 19961007 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Memorandum 4727 Pilot Evaluations of Runway Status Light System Steven D. Young, Robert W. Wills, and R. Marshall Smith Langley Research Center Hampton, Virginia October 1996 Printed copies
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-aiaa-95-3619.ps.Z, 19961008 For permission to copy or republish, contact the American Institue of Aeronautics and Astronautics1801 Alexander Bell Drive, Suite 500, Reston, VA 22091AIAA 95-3619Defining Support RequirementsDuring Conceptual Design ofReusable Launch VehiclesW. D. MorrisN. H.WhiteW.T. DavisNASA Langley Research
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-1991.ps.Z, 19961008 1
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-ncnce-yyt.ps.Z, 19961011 Last name: Tang Page number: MODELING OF SOUND TRANSMISSION THROUGH SHELL STRUCTURES WITH TURBULENT BOUNDARY LAYER EXCITATION Yvette Y. Tang, Research Associate National Research Council MS 463, NASA Langley Research Center, Hampton, VA 23681 Richard J. Silcox, Assistant Branch Head Jay H. Robinson,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-amtas-rlc.ps.Z, 19961016 EVALUATION OF COMPLEX PERMITTIVITIES OF MULTILAYER DIELECTRIC SUBSTRATES AT MICROWAVE FREQUENCIES USING WAVEGUIDE MEASUREMENTS 1 R. L. Cravey1, M. D. Deshpande2, C. J. Reddy3, and P. I. Tiemsin1 (1) NASA Langley Research Center, Hampton, Virginia 23681 (2) ViGYAN Inc.,, Hampton, Virginia 23681 (3)
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-0292.ps.Z, 19961016 For permission to copy or republish, contact the American Institute of Aeronautics and Astronautics370 L'Enfant Promenade, S.W., Washington, D.C. 20024AIAA-96-0292Assessment of an Unstructured-Grid Methodfor Predicting 3-D Turbulent Viscous FlowsN. T. FrinkNASA Langley Research CenterHampton, VA34th
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-cr4758.ps.Z, 19961018 NASA Contractor Report 4758Application of AWE for RCS frequencyresponse calculations using Method ofMomentsC.J.ReddyHampton University, Hampton, VirginiaM.D.DeshpandeViGYAN Inc., Hampton, VirginiaOctober 1996National Aeronautics andSpace AdministrationLangley Research CenterHampton, Virginia 23681-0001
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tp3594.ps.Z, 19961018 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3594 Study of Analytic Statistical Model for Decay of Light and Medium Mass Nuclei in Nuclear Fragmentation Francis A. Cucinotta and John W. Wilson Langley Research Center Hampton,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tp3597.ps.Z, 19961021 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3597 Subsonic Analysis of 0.04-Scale F-16XL Models Using an Unstructured Euler Code Wendy B. Lessard Langley Research Center Hampton, Virginia October 1996 Printed copies available
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-14assm-arj.ps.Z, 19961023 1 Viscous Effects in the Elastodynamics of Thick Beams A. R. Johnson1 and A. Tessler Computational Structures Branch NASA Langley Research Center, MS240 Hampton, VA 23681-0001 Summary A viscoelastic higher-order thick beam finite element formulation is extended to include elastodynamic deformations. The
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-17asem-bdj.ps.Z, 19961024 A FRAMEWORK FOR THE OPTIMIZATION OF DISCRETE- EVENT SIMULATION MODELS B. D. Joshi#, R. Unal#, N. H. White* and W. D. Morris* # Dept. of Engineering Management * Vehicle Analysis Branch Old Dominion University NASA Langley Research Center Norfolk, VA 23529 Hampton, VA 23681 Presented at the 17th ASEM
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-4181.ps.Z, 19961024 1 Optimization of Operations Resources via Discrete Event Simulation Modeling B. Joshi#, D. Morris, N. White and R. Unal# # Dept. of Engineering Management *Vehicle Analysis Branch Old Dominion University NASA Langely Research Center Norfolk, VA 23529 Hampton, VA 23681 Presented at the 6th
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-17asem.bdj.ps.Z, 19961024 A FRAMEWORK FOR THE OPTIMIZATION OF DISCRETE- EVENT SIMULATION MODELS B. D. Joshi#, R. Unal#, N. H. White* and W. D. Morris* # Dept. of Engineering Management * Vehicle Analysis Branch Old Dominion University NASA Langley Research Center Norfolk, VA 23529 Hampton, VA 23681 Presented at the 17th ASEM
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm109039.ps.Z, 19961030 NASA Technical Memorandum 109039 FREQUENCY DOMAIN IDENTIFICATION TOOLBOX Lucas G. Horta and Jer-Nan Juang NASA Langley Research Center Hampton, Virginia 23681-0001 Chung-Wen Chen North Carolina State University Raleigh, NC 27695-7910 September 1996 National Aeronautics and Space Administration Langley
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4724.ps.Z, 19961031 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Memorandum 4724 Progressive Damage Analysis of Laminated Composite (PDALC) A Computational Model Implemented in the NASA COMET Finite Element Code David C. Lo Texas A&M University College
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tp3618.ps.Z, 19961101 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3618 A Combined FEM/MoM/GTD Technique To Analyze Elliptically Polarized Cavity-Backed Antennas With Finite Ground Plane C. J. Reddy Hampton University Hampton, Virginia M. D. Deshpande
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-cr4755.ps.Z, 19961101 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-0001NASA Contractor Report 4755Real-Gas Flow Properties for NASA LangleyResearch Center Aerothermodynamic FacilitiesComplex Wind TunnelsBrian R. HollisNorth Carolina State University Raleigh, North
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-4589.ps.Z, 19961104 AIAA 96-4589 1 Analytic Corrections to CFD Heating Predictions Accounting for Changes in Surface Catalysis, Part II Peter A. Gnoffo NASA Langley Research Center Hampton, Virginia 23681-0001 and George R. Ingery Iowa State University Ames, Iowa 50011-3231
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-4245.ps.Z, 19961104 For permission to copy or republish, contact the American Institue of Aeronautics and Astronautics 1801 Alexander Bell Drive, Suite 500, Reston, VA 22091 AIAA 96-4245 Analysis of Shuttle Orbiter Reliability and Maintainability Data for Conceptual Studies W. D. Morris N. H. White NASA Langley Research
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-4138.ps.Z, 19961104 A SURROGATE APPROACH TO THE EXPERIMENTAL OPTIMIZATION OF MULTIELEMENT AIRFOILS John C. Otto Multidisciplinary Optimization Branch NASA Langley Research Center Hampton, Virginia Department of Aeronautics and Astronautics, M.I.T. Drew Landmany Department of Engineering Technology Old Dominion University
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-cr201607.ps.Z, 19961105 NASA Contractor Report 201607 DOT/FAA/ND-96/2 Performance of the NASA Airborne Radar With the Windshear Database for Forward-Looking Systems George F. Switzer and Charles L. Britt Research Triangle Institute, Research Triangle Park, North Carolina Contract NAS1-18925 September 1996 National Aeronautics
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tp3601.ps.Z, 19961106 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3601 A Guidance Scheme for Automated Tetrahedral Truss Structure Assembly Based on Machine Vision William R. Doggett Langley Research Center Hampton, Virginia November 1996 Printed
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3428.ps.Z, 19961107 NASATechnical Paper 3428IntroductiontoGeneralized Functions WithApplicationsinAerodynamicsandAeroacousticsF.FarassatLangley ResearchCenterfflHampton,VirginiaCorrectedCopy (April1996)NationalAeronautics and Space AdministrationLangleyResearchCenterfflHampton, Virginia23681-0001May1994 ContentsSymb
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-cr4756.ps.Z, 19961107 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-0001NASA Contractor Report 4756Validation Tests of TASS for Application to 3-DVortex SimulationsGeorge F. SwitzerResearch Triangle Institute Research Triangle Park, North CarolinaOctober 1996Prepared for Langley
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3399.ps.Z, 19961108 NASATechnicalPaper33991993Final-Approach SpacingAids(FASA)Evaluation ForTerminal-Area,Time-BasedAir TrafficControlLeonardCredeurLangleyResearchCenterHampton,VirginiaWilliamR.CapronLockheedEngineering&SciencesCompanyHampton,VirginiaGary W.LohrEmbry-RiddleAeronauticalUniversityDaytonaBeach,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-4098.ps.Z, 19961112 1 AIAA-CP-4098 DISPLACEMENT BASED MULTILEVEL STRUCTURAL OPTIMIZATION A. G. Striz School of Aerospace and Mechanical Engineering The University of Oklahoma Norman, Oklahoma 73019-0601 405-325-1730, e-mail striz@uoknor.edu J. Sobieszczanski-Sobieski MDO Coordinator NASA Langley Research Center Hampton,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/aiaa-93-3009.ps.Z, 19961125 ACOMPUTATIONALAND EXPERIMENTAL INVESTIGATIONOF A DELTAWING WITH VERTICALTAILSSherrie L. KristandAnthonyE.WashburnViGYAN,Inc.Hampton,VirginiaKennethD. Visser NationalResearch CouncilHampton,VirginiaABSTRACTTheflowoveranaspectratio1deltawingwithtwinverticaltailsisstudied in a combined computationaland
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/NASA-aiaa-97-0057.ps.Z, 19961126 NASA WAKE VORTEX RESEARCH FOR AIRCRAFT SPACING R. Brad Perry, David A. Hinton, and Robert A. Stuever** NASA Langley Research Center Hampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/97/NASA-aiaa-97-0057.ps.Z, 19961126 NASA WAKE VORTEX RESEARCH FOR AIRCRAFT SPACING R. Brad Perry, David A. Hinton, and Robert A. Stuever** NASA Langley Research Center Hampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110292.ps.Z, 19961127 1NASA Technical Memorandum 110292Asymptotic Waveform Evaluation(AWE)Technique for Frequency DomainElectromagnetic AnalysisC. R. Cockrell and F.B. BeckNASA Langley Research Center, Hampton, VirginiaNovember 1996National Aeronautics andSpace AdministrationLangley Research CenterHampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/NASA-97-1psfvip-lmw.ps.Z, 19961203 VISUALIZATION AND IMAGE PROCESSING OF AIRCRAFT SHOCK WAVE STRUCTURESLeonard M. WeinsteinMeasurement Science and Technology BranchNASA Langley Research CenterHampton, VirginiaUSA Kathryn StacyScientific Applications BranchNASA Langley Research CenterHampton, VirginiaUSA Gerald J. VieiraSounding Rockets
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110294.ps.Z, 19961203 NASA Technical Memorandum 110294 User s Guide for Flight Simulation Data Visualization Workstation Joseph A. Kaplan and Ronnie Chen Langley Research Center Hampton, Virginia Patrick S. Kenney, Christopher M. Koval, and Brian K. Hutchinson UNISYS Corporation Hampton, Virginia November 1996 National
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/97/NASA-97-1psfvip-lmw.ps.Z, 19961203 VISUALIZATION AND IMAGE PROCESSING OF AIRCRAFT SHOCK WAVE STRUCTURESLeonard M. WeinsteinMeasurement Science and Technology BranchNASA Langley Research CenterHampton, VirginiaUSA Kathryn StacyScientific Applications BranchNASA Langley Research CenterHampton, VirginiaUSA Gerald J. VieiraSounding Rockets
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-cr198297.ps.Z, 19961203 NASA Contractor Report 198297 (Corrected Copy Dec. 1996) Turbulent Wall-Pressure Fluctuations: New Model for Off-Axis Cross-Spectral Density Bart A. Singer High Technology Corporation, Hampton, Virginia Contract NAS1-20059 March 1996 National Aeronautics and Space Administration Langley Research Center
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110250.ps.Z, 19961204 The Influence of Lamination Angles on the Interior Noise Levels of an Aircraft Christian M. Fernholz Ford Motor Company, Dearborn, MI Jay H. Robinson NASA Langley Research Center, Hampton, VA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110286.ps.Z, 19961206 NASA Technical Memorandum 110286Properties of Two Carbon Composite Materials Using LTM25 Epoxy ResinJuan R. CruzLangley Research Center, Hampton, VirginiaC. H. Shah and A. S. PostynNorthrop Grumman Corporation, El Segundo, CaliforniaNovember 1996National Aeronautics andSpace AdministrationLangley
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110295.ps.Z, 19961209 NASA Technical Memorandum 110295Investigation of Low-Reynolds-Number Rocket Nozzle Design Using PNS-Based Optimization ProcedureM. Moin Hussaini and John J. KorteLangley Research Center, Hampton, VirginiaNovember 1996National Aeronautics andSpace AdministrationLangley Research CenterHampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-jpjsm-dfp.ps.Z, 19961212 APortable Surface Contamination Monitor Based on the Principle of Optically Stimulated Electron Emission (OSEE)ByD. F. PereyNASALangley Research CenterMail Stop 231Hampton, VA23681ABSTRACTMany industrial and aerospace processes involving the joining of materials, require sufficient surfacecleanliness to
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110296.ps.Z, 19961212 NASA Technical Memorandum 110296 Development of Metallic Thermal Protection Systems for the Reusable Launch Vehicle Max L. Blosser Langley Research Center, Hampton, Virginia October 1996 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 1 DEVELOPMENT OF
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/NASA-aiaa-97-0297.ps.Z, 19961213 1 ENHANCED CONTROL EFFECTOR DESIGNS FOR AIRBREATHING TRANSATMOSPHERIC VEHICLES Charles E. Cockrell, Jr.* and John D. McMinn= NASA Langley Research Center, Hampton, VA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/97/NASA-aiaa-97-0297.ps.Z, 19961213 1 ENHANCED CONTROL EFFECTOR DESIGNS FOR AIRBREATHING TRANSATMOSPHERIC VEHICLES Charles E. Cockrell, Jr.* and John D. McMinn= NASA Langley Research Center, Hampton, VA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4750.ps.Z, 19961216 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Memorandum 4750 Utilizing GPS To Determine Ionospheric Delay Over the Ocean Stephen J. Katzberg and James L. Garrison, Jr. Langley Research Center Hampton, Virginia December 1996 Printed
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4741.ps.Z, 19961217 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Memorandum 4741 Computer Program To Obtain Ordinates for NACA Airfoils Charles L. Ladson, Cuyler W. Brooks, Jr., and Acquilla S. Hill Langley Research Center Hampton, Virginia Darrell W.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-jam-mrg.ps.Z, 19961217 Application of Normal Mode Expansion to AE Waves in Finite Plates1 M. R. Gorman2 and W. H. Prosser3 INTRODUCTION Breckenridge et al. (1975), Hsu (1985) and Pao (1978) adapted approaches from seismology to calculate the response at the surface of an infinite half-space and an infinite plate. These
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tp3616.ps.Z, 19961217 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3616 Nonlinear Analysis of the Space Shuttle Superlightweight External Fuel Tank Michael P. Nemeth, Vicki O. Britt, Timothy J. Collins, and James H. Starnes, Jr. Langley Research
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110290.ps.Z, 19961217 Integration of Multiple Non-Normal Checklist Procedures into a Single Checklist Procedure for Transport Aircraft - A Preliminary Investigation Lynda J. Foernsler Crew/Vehicle Integration Branch Flight Dynamics and Control Division i
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-ai96p-dmb.ps.Z, 19961218 ADVANCED CIVILIAN AERONAUTICAL CONCEPTS Dennis M. Bushnell NASA - Langley Research Center - U.S.A.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-cr4761.ps.Z, 19961218 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-0001NASA Contractor Report 4761Preparation and Properties of High-TcBi-Pb-Sr-Ca-Cu-O Thick Film Superconductorson YSZ SubstratesMatthew W. HookerLockheed Martin Engineering & Sciences Company Hampton,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm4673.ps.Z, 19961219 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Memorandum 4673 Surface-Pressure and Flow-Visualization Data at Mach Number of 1.60 for Three 65 Delta Wings Varying in Leading-Edge Radius and Camber S. Naomi McMillin Langley Research
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-cnde-whp.ps.Z, 19961220 Proceedings of the SPIE Conference on Nondestructive Evaluation Techniques for Aging Infrastructureand Manufacturing: Materials and Composites, December 2-5, 1996, Scottsdale, Arizona, pp. 146-153.Applications of Advanced, Waveform Based AE Techniques for Testing Composite MaterialsWilliam H.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-jfe-rdj.ps.Z, 19961220 Active Control of Instabilities in Laminar Boundary Layers{ Overview and Concept Validation Ronald D. Joslin,1 Gordon Erlebacher,2 and M. Yousuff Hussaini3
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-14assm-kej.ps.Z, 19961220 Proceedings of the 14 th U.S. Army Symposium on Solid Mechanics Damage Initiation and Ultimate Tensile Strength of Scaled T GraphiteEpoxy Coupons Karen E. Jackson US Army Research Laboratory, Vehicle Structures Directorate NASA Langley Research Center Hampton, VA William H. Prosser
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-fdr-rdj.ps.Z, 19961220 Simulation of nonlinear instabilities in an attachment-line boundary layer Ronald D. Joslin NASA Langley Research Center, Hampton, Virginia 23681, U.S.A.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tp3610.ps.Z, 19970106 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3610 Calibration of NASA Turbulent Air Motion Measurement System John D. W. Barrick, John A. Ritter, Catherine E. Watson, Mark W. Wynkoop, John K. Quinn, and Daniel R. Norfolk Langley
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/NASA-97-tm4744.ps.Z, 19970106 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Memorandum 4744 A Comparison of Two Control Display Unit Concepts on Flight Management System Training Terence S. Abbott Langley Research Center Hampton, Virginia January 1997 Printed copies
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-aiaaj-wrw.ps.Z, 19970108 VALIDATION OF A NUMERICAL METHOD FOR DETERMINING LINER IMPEDANCE Willie R. Watson NASA Langley Research Center, Hampton Virginia Michael G. Jonesy Lockheed Engineering & Sciences Company, Hampton Virginia Sharon E. Tannerz And Tony L. Parrottz NASA Langley Research Center, Hampton Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-cr201635.ps.Z, 19970109 1NASA Contractor Report 201635A DESCRIPTION OF THE SOFTWARE ELEMENT OF THE NASA EMEFLIGHT TESTSSandra V. KoppenLockheed Martin Engineering & Sciences Company, Hampton, Virginia 23666Contract: NAS1-19000December 1996National Aeronautics andSpace AdministrationLangley Research CenterHampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/NASA-97-ac-rdb.ps.Z, 19970110 Mars Microprobe Entry Analysis Robert D. Braun NASA Langley Research Center Hampton, VA 23681-0001 (757) 864-4507 r.d.braun@larc.nasa.gov Robert A. Mitcheltreey NASA Langley Research Center Hampton, VA 23681-0001 (757) 864-4382 r.a.mitcheltree@larc.nasa.gov F. McNeil Cheatwood Vigyan Inc. Hampton, VA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-mrs-zo.ps.Z, 19970113 DIELECTRIC PROPERTIES OF PIEZOELECTRIC POLYIMIDES Z. OUNAIES1, J. A. YOUNG2, J. O. SIMPSON3, B. L. FARMER2 1National Research Council, NASA Langley Research Center, Hampton, VA 23681 2 University of Virginia, Department of Materials Science and Engineering, Charlottesville, VA 22903 3Composites and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-ja-wka.ps.Z, 19970114 ANDERSON ET AL.: NAVIER-STOKES COMPUTATIONS Navier-Stokes Computations and Experimental Comparisons for Multielement Airfoil Configurations W. Kyle Anderson,Daryl L. Bonhaus,Robert McGhee, and Betty Walker NASA Langley Research Center Hampton, VA 23681
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-jcp-wka.ps.Z, 19970114 AIAA 95-1740 1 Implicit/Multigrid Algorithms for Incompressible Turbulent Flows on Unstructured Grids W. Kyle Anderson,* Russ D. Rausch, Daryl L. Bonhaus NASA Langley Research Center, Hampton, Virginia 23681 Summary An implicit code for computing inviscid and viscous incompressible flows on unstructured
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/NASA-97-tp3621.ps.Z, 19970114 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3621 Universal Parameterization of Absorption Cross Sections R. K. Tripathi Southern Illinois University Carbondale, Illinois Francis A. Cucinotta and John W. Wilson Langley Research
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/NASA-aiaa-97-0056.ps.Z, 19970115 Copyright 1997 by the American Institute of Aeronautics, Inc. No copyright is asserted in the Un ited States under Title 17,U .S. Code. The U.S. Government has a royalty-free license to exercise all rights under the copyright claimed herin forgovernment purposes. All other rights are reserved by the
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110285.ps.Z, 19970116 NASA Technical Memorandum 110285The Kirchhoff Formulas for MovingSurfaces in Aeroacoustics - The Subsonicand Supersonic CasesF. FarassatLangley Research Center, Hampton, VirginiaSeptember 1996National Aeronautics andSpace AdministrationLangley Research CenterHampton, Virginia 23681-0001 THE KIRCHHOFF
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110291.ps.Z, 19970116 NASA Technical Memorandum 110291A Benchmark Problem For Development of Autonomous Structural Modal IndentificationRichard S. Pappa, Stanley E. Woodard, and Jer-Nan JuangLangley Research Center, Hampton, VirginiaOctober 1996National Aeronautics andSpace AdministrationLangley Research CenterHampton,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/NASA-92-tm107691.ps.Z, 19970117 NASA Technical Memorandum 107691 Modeling and Model Simplification of Aeroelastic Vehicles: An Overview Martin R. Waszak and Carey S. Buttrill Langley Research Center Hampton, Virginia David K. Schmidt Arizona State University Tempe, Arizona September 1992 Modeling and Model Simplification of
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-3362.ps.Z, 19970117 AIAA Paper No. 96-3362 - AIAA Atmospheric Flight Mechanics Conference PARAMETER ESTIMATION AND ANALYSIS OF ACTUATORS FOR THE BACT WIND-TUNNEL MODEL Martin R. Waszak* and Jimmy Fung, NASA Langley Research Center, Hampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/NASA-aiaa-97-0829.ps.Z, 19970117 1 American Institute of Aeronautics and Astronautics THE BENCHMARK ACTIVE CONTROLS TECHNOLOGY MODEL AERODYNAMIC DATA Robert C. Scott*, Sherwood T. Hoadley , Carol D. Wieseman , and Michael H. Durham NASA Langley Research Center Hampton, VA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-3437.ps.Z, 19970117 AIAA Paper No. 96-3437 - AIAA Atmospheric Flight Mechanics Conference MODELING THE BENCHMARK ACTIVE CONTROL TECHNOLOGY WIND- TUNNEL MODEL FOR APPLICATION TO FLUTTER SUPPRESSION Martin R. Waszak,* NASA Langley Research Center, Hampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3198.ps.Z, 19970121 NASATechnical Paper 3198SoftwareDesign forAutomated AssemblyofTruss StructuresCatherineL.Herstrom, CarolynGrantham,CherylL.Allen,William R.Doggett,and RalphW.WillLangley ResearchCenterfflHampton,VirginiaNationalAeronautics and Space AdministrationLangleyResearchCenterfflHampton,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110298.ps.Z, 19970122 NASA Technical Memorandum 110298U. S. Army Research Laboratory Technical Report 1288Finite-Element Vibration Analysis and Modal Testing of Graphite Epoxy Tubes and Correlation Between the DataBarmac K. TaleghaniVehicle Structures DirectorateU.S. Army Research LaboratoryLangley Research Center, Hampton,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/NASA-94-candf-wka.ps.Z, 19970123 Computers Fluids Vol. 23, No. 1, pp. 1 21, 1994 An Implicit Upwind Algorithm for Computing Turbulent Flows on Unstructured Grids. W. Kyle Anderson and Daryl L. Bonhaus NASA Langley Research Center Hampton, Virginia 23665 5225 An implicit, Navier-Stokes solution algorithm is presented for the computation
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110308.ps.Z, 19970123 NASA Technical Memorandum 110308 Development of a Flight Simulation Data Visualization Workstation Joseph A. Kaplan and Ronnie Chen Langley Research Center Hampton, Virginia Patrick S. Kenney, Christopher M. Koval, and Brian K. Hutchinson UNISYS Corporation Hampton, Virginia December 1996 National
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/NASA-aiaa-97-0643.ps.Z, 19970123 AIAA 95-17401Implicit/Multigrid Algorithms for Incompressible TurbulentFlows on Unstructured GridsW. Kyle Anderson,* Russ D. Rausch, Daryl L. Bonhaus NASA Langley Research Center, Hampton, Virginia 23681SummaryAn implicit code for computing inviscid and viscous incompressible flows on unstructured grids
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-asme-wkw.ps.Z, 19970124 AEROELASTIC ANALYSIS OF HELICOPTER ROTOR BLADES INCORPORATING ANISOTROPICPIEZOELECTRIC TWIST ACTUATIONW. Keats Wilkie W. Keith BelvinNASA Langley Research Center NASA Langley Research CenterAeroelasticity Branch Structural Dynamics BranchMail Stop 340 Mail Stop 230Hampton, Virginia 23681-0001, U.S.A.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/NASA-97-tp3623.ps.Z, 19970127 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3623 Direct Numerical Simulation of Evolution and Control of Linear and Nonlinear Disturbances in Three-Dimensional Attachment-Line Boundary Layers Ronald D. Joslin Langley Research
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/NASA-aiaa-97-0244.ps.Z, 19970128 VALIDATION OF AN EXPERIMENTALLY DERIVED UNCERTAINTY MODEL K.B. Lim , D.E. Coxy, G.J. Balaszand J-N. Juangx The results show that uncertainty models can be obtained directly from system identification data by using a minimum norm model validation approach. The error between the test data and an
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/NASA-aiaa-97-0750.ps.Z, 19970204 AIAA97-0750Large-EddySimulationofLaminar-TurbulentTrans itioninaSwept-WingBoundaryLayerX. HuaiUniversity of MarylandCollege Park, MDR. D. JoslinNASA Langley Research CenterHampton, VA; andU. PiomelliUniversity of MarylandCollege Park, MD
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/aiaa/NASA-aiaa-97-0868.ps.Z, 19970205 AIAA-97-0868Computation of Thermally Perfect ObliqueflShock Wave Properties35th Aerospace SciencesflMeeting & ExhibitJanuary 6-10, 1997 / Reno, NVKenneth E. TatumflLockheed Martin Engineering & Sciences, flHampton, VA 1American Institute of Aeronautics and AstronauticsAIAA-97-0868Computation of
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/NASA-97-tp3586.ps.Z, 19970206 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3586 Quasi-Static and Dynamic Response Characteristics of F-4 Bias-Ply and Radial-Belted Main Gear Tires Pamela A. Davis Langley Research Center Hampton, Virginia February 1997 Printed
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/NASA-97-tp3638.ps.Z, 19970210 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3638 Expanded Equations for Torque and Force on a Cylindrical Permanent Magnet Core in a Large- Gap Magnetic Suspension System Nelson J. Groom Langley Research Center Hampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/NASA-97-9ams-abc.ps.Z, 19970210 P2.7 EVALUATION OF TIME-AVERAGED CERES TOA SW PRODUCT USING CAGEX DATA Ann B. Carlson* and Takmeng Wong Atmospheric Sciences Division, Langley Research Center, NASA Hampton, VA 1. INTRODUCTION A major component in the analysis of the Earth s radiation budget is the recovery of daily and monthly averaged
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/NASA-97-cr201653.ps.Z, 19970211 NASA Contractor Report 201653 A Users' Manual and Tutorial for Performing COMET Structural Analyses Using an Advanced User-Friendly Interface Charles L. Blackburn, Christine G. Lotts, and Brian H. Mason Analytical Services and Materials, Inc., Hampton, Virginia Contract NAS1-19700 January 1997 National
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-jgcd-kbl.ps.Z, 19970212 HANKEL SINGULAR VALUES OF FLEXIBLE STRUCTURES IN DISCRETE TIME K.B. Lim NASA Langley Research Center W. Gawronskiy Jet Propulsion Laboratory, California Institute of Technology
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/NASA-97-ispqi-sjb.ps.Z, 19970214 RF #97RM-102: RF1Aerospace Applications of Weibulland Monte Carlo Simulationwith Importance SamplingSalvatore J. Bavuso; NASA; HamptonKey Words: Weibull, Reliability, Monte Carlo, simulation, importance sampling, HARP (Hybrid Automated Reliability Prediction), Fault tree, HIRel (HARP integrated
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr201681fldup.ps.Z, 19970226 92 User User Application Analysis Application Catalog Services Security Services Driver Application Model Application 1: Display login screen 2: Enter ID and password 3: Authenticate user 7: User role OK 8: Connect 9: Connect OK 10: Display analysis interface 4: Authenticate user 6: User role OK 5:
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm110244.ps.Z, 19970321 NASA Technical Memorandum 110244 Neural Generalized Predictive Control: A Newton-Raphson Implementation Donald Soloway and Pamela J. Haley Langley Research Center, Hampton, Virginia February 1997 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 1 NEURAL
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-4sssm-saw.ps.Z, 19970324 1
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm110316.ps.Z, 19970324 NASA Technical Memorandum 110316 Virtual Passive Controller for Robot Systems Using Joint Torque Sensors Hal A. Aldridge and Jer-Nan Juang Langley Research Center, Hampton, Virginia January 1997 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 Virtual
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/aiaa/NASA-aiaa-97-0625.ps.Z, 19970325 97{0625 HYPERSONIC FLOW COMPUTATIONS ON UNSTRUCTURED MESHES K. L. Bibb NASA Langley Research Center, Hampton, VA 23681 J. Perairey Massachusetts Institute of Technology, Cambridge, MA 02139 C. J. Rileyz NASA Langley Research Center, Hampton, VA 23681 A method for computing inviscid hypersonic flow over
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm110314.ps.Z, 19970326 NASA Technical Memorandum 110314Robot Position Sensor Fault ToleranceHal A. AldridgeLangley Research Center, Hampton, VirginiaJanuary 1997National Aeronautics andSpace AdministrationLangley Research CenterHampton, Virginia 23681-0001 iTable of Contents1. INTRODUCTION AND LITERATURE
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/aiaa/NASA-aiaa-97-0108.ps.Z, 19970326 STABILITY ANALYSIS FOR CONSTRAINED PRINCIPAL AXIS SLEW MANEUVERS Hans Seywald Analytical Mechanics Associates Hampton VA seywald@scb2.larc.nasa.gov Kyong B. Limy NASA Langley Research Center Hampton VA k.b.lim@larc.nasa.gov Tobin C. Anthonyz NASA Goddard Space Flight Center Greenbelt, MD
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm4753.ps.Z, 19970331 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Memorandum 4753 Multilayer Analyses of an Iron Radiation Beam Experiment J. L. Shinn and J. W. Wilson Langley Research Center Hampton, Virginia E. V. Benton University of San Francisco San
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-aas-97-195.ps.Z, 19970406 AAS 97-195 ON THE POSSIBILITY OF ILL-CONDITIONED COVARIANCE MATRICES IN THE FIRST-ORDER TWO-STEP ESTIMATOR James L. Garrison 1 Penina Axelrad 2 N. Jeremy Kasdin 3 The first-order two-step nonlinear estimator, when applied to a problem of orbital navigation, is found to occasionally produce first step
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/NASA-94-tm109130.ps.Z, 19970407 NASA Technical Memorandum 109130 Gain Weighted Eigenspace Assignment John B. Davidson NASA Langley Research Center, Hampton, Virginia Dominick Andrisani, II Purdue University, West Lafayette, Indiana May 1994 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-iceaf-jcn.ps.Z, 19970411 Engineering Against Fatigue, University of Sheffield, March 1997 Prediction of Crack Growth under Variable-Amplitude Loading in Thin-Sheet 2024-T3 Aluminum Alloys J. C. Newman, Jr. NASA Langley Research Center Hampton, Virginia, USA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tp/NASA-97-tp3604.ps.Z, 19970411 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3604 Exploratory Investigation of Forebody Strakes for Yaw Control of a Generic Fighter With a Symmetric 60 Half-Angle Chine Forebody Holly M. Ross Langley Research Center Hampton,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tp/NASA-97-tp3643.ps.Z, 19970411 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3643 Astronaut Protection From Solar Event of August 4, 1972 John W. Wilson and Francis A. Cucinotta Langley Research Center Hampton, Virginia T. D. Jones Oak Ridge National Laboratory
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tp/NASA-97-tp3605.ps.Z, 19970411 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3605 A Study of Fundamental Shock Noise Mechanisms Kristine R. Meadows Langley Research Center Hampton, Virginia April 1997 Printed copies available from the following: NASA Center for
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-ieeesecon-jlg.ps.Z, 19970414 DETECTION OF OCEAN REFLECTED GPS SIGNALS: THEORY AND EXPERIMENT James L. Garrison y, Stephen J. Katzberg MS 328 - Spacecraft and Sensors Branch NASA Langley Research Center, Hampton, VA y (757)864-4441 j.l.garrison@larc.nasa.gov Charles T. Howell III Lockheed Martin Engineering & Sciences Co., Hampton,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr4773.ps.Z, 19970414 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-0001NASA Contractor Report 4773ERBE Geographic Scene and Monthly SnowDataLisa H. Coleman, Beth T. Flug, Shalini Gupta, Edward A. Kizer, and John L. RobbinsScience Applications International Corporation Hampton,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-13race-kwh.ps.Z, 19970415 Computational Diagnostic Techniques for Electromagnetic Scattering:Analytical Imaging, Near Fields, and Surface CurrentsKam W. Hom, Noel A. Talcott, Jr.NASA Langley Research CenterHampton, Virginia 23665John ShaefferMarietta Scientific, Inc.376 Powder Springs St., Suite 240AMarietta, Georgia 30064(770)
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tp/NASA-97-tp3640.ps.Z, 19970416 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3640 Electromagnetic Scattering From Arbitrarily Shaped Aperture Backed by Rectangular Cavity Recessed in Infinite Ground Plane C. R. Cockrell and Fred B. Beck Langley Research Center
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm110338.ps.Z, 19970416 NASA Technical Memorandum 110338 An Application of the Difference Potentials Method to Solving External Problems in CFD Victor S. Ryaben'kii Keldysh Institute for Applied Mathematics Russian Academy of Sciences, Moscow, Russia Semyon V. Tsynkov Langley Research Center, Hampton, Virginia March 1997
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-acs-gam.ps.Z, 19970418 The Wettability of LaRC Colorless Polyimide Resins on Casting Surfaces Gilda A. Miner, Diane M. Stoakley, Anne K. St. Clair, NASA Langley Research Center, Hampton, VA 23681-0001; Paul A. Gierow, and Kevin Bates SRS Technologies, 500 Discovery Drive, Huntsville, AL 35806 INTRODUCTION Two colorless
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/aiaa/NASA-aiaa-97-1305.ps.Z, 19970418 Copyright 1997 by the American Institute of Aeronautics andAstronautics, INC. No copyright is asserted in the United States underTitle 17, U.S. Code. The U.S. Government has a royalty-free license toexercise all rights under the copyright claimed herein for governmentpurposes. All other rights are
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm110337.ps.Z, 19970421 NASA Technical Memorandum 110337 External Boundary Conditions for Three-Dimensional Problems of Computational Aerodynamics Semyon V. Tsynkov Langley Research Center, Hampton, Virginia March 1997 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 EXTERNAL
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr4767.ps.Z, 19970421 NASA Contractor Report 4767Documentation of Atmospheric ConditionsDuring Observed Rising Aircraft WakesJ. Allen ZakViGYAN, Inc. Hampton, VirginiaWilliam G. Rodgers, Jr.Lockheed Martin Engineering and Sciences Hampton, VirginiaApril 1997Prepared for Langley Research Centerunder Contract NAS1-96014
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm110329.ps.Z, 19970421 NASA Technical Memorandum 110329Subsonic Dynamics of Stardust Sample Return CapsuleR. A. Mitcheltree and C. M. FremauxLangley Research Center, Hampton, VirginiaMarch 1997National Aeronautics andSpace AdministrationLangley Research CenterHampton, Virginia 23681-0001 Subsonic Dynamics of Stardust Sample
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr201678.ps.Z, 19970422 NASA Contractor Report 201678The ASAC Air Carrier Investment Model(Second Generation)Earl R. Wingrove III and Jesse P. JohnsonLogistics Management Institute, McLean, VirginiaRobin G. SicklesRice University, Houston, TexasDavid H. GoodIndiana University, Bloomington, IndianaContract NAS2-14361April
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-agard-jjk.ps.Z, 19970423 C-40-1MULTIDISCIPLINARY OPTIMIZATION METHODSFOR PRELIMINARY DESIGNJ. J. Korte, R. P. Weston, and T. A. ZangMultidisciplinary Optimization Branch, MS 159NASA Langley Research CenterHampton, VA 23681-0001 USASUMMARYAn overview of multidisciplinary optimization (MDO)methodology and two applications of this
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm110339.ps.Z, 19970425 NASA Technical Memorandum 110339 Computation of Sound Generated by Viscous Flow Over a Circular Cylinder Jared S. Cox The George Washington University Joint Institute for Advancement of Flight Sciences Langley Research Center, Hampton, Virginia Christopher L. Rumsey and Kenneth S. Brentner Langley
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3145.ps.Z, 19970428 NASATechnical Paper 3145ThermalandStructuralTestsof Rene 41Honeycomb Integral-TankConceptfor FutureSpace Transportation SystemsJohnL.Shideler,RogerA.Fields,LawrenceF.Reardon,andLeslieGongMay1992 Theuse of trademark s or names of manufacturers inthisre portisforacc uratereportinganddoes not constitute
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3126.ps.Z, 19970428 NASATechnical Paper 3126EffectofCrashPulse Shape onScatStrokeRequirementsforLimitingLoadson Occupantsof AircraftHueyD.CardenFebruary1992 SummaryAn analyticalstudywas mad eto(1)providecom-parativeinformation onvarious crashpulseshapesthatpotentiallycould beusedtotestseats tothe pa-ra meter conditions
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3150.ps.Z, 19970428 NASATechnical Paper 3150FeasibilityStudy ofaLow-Energy Gamma RaySystem forMeasuringQuantity and FlowRateof SlushHydrogenJag J.Singh,Chih-PingShen, andDanny R.SprinkleApril 1992 Ab stractAs part ofastudy todemonstratethe suitabil-it y of anX-rayorgammaray probe formonitoringthe quantity and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3157.ps.Z, 19970428 NASATechnical Paper 3157SimulationofReal-Gas EffectsonPressureDistributionsfor Aeroassist Flight ExperimentVehicle and ComparisonWithPredictionJohnR.MicolApril 1992 SummaryTheAeroassist Flight Exp eriment(AFE)utilizesa14-ft-diameterrakedandb lunted ellip ticconeasavehi cleto carryinstrumentation for10
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3131.ps.Z, 19970428 NASATechnical Paper 3131Two-DimensionalStabilityofLaminar FlamesH. S.Mukunda and J. PhilipDrummondJanuary 1992 SymbolsAbfrequencyfactorforbackwardreactionAffrequencyfactorforforward reactionc pspecificheat atconstantpressureDdiffusioncoefficientEactivation energyhctheatofcombustionof reactionhienthalpy
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3132.ps.Z, 19970428 NASATechnical Paper 3132Comparison ofaTwoDimensionalAdaptiveWallTechniqueWithAnalytical WallInterference Correction TechniquesRaymondE.MineckApril 1992 Comp arisonsofthechordw isepre ssuredistributionsat near ly the samenorma l-force coefficient and Machnumberare presentedin aSupplementtoN
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3147.ps.Z, 19970428 NASATechnical Paper 3147An Efficient HZETRN(A Galactic CosmicRayTransport Code)JudyL.ShinnandJohnW. WilsonApril 1992 AbstractTo meetthe challengeofthefuturedeep-spaceprogram,whichinvolvese xtendedmanned spacemissions,anaccurateandefficiente ngineeringcodefor analyzingthe shielding require
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm4754.ps.Z, 19970429 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Memorandum 4754 ARL Technical Report 1283 ATCOM Technical Report 97-A-006 Performance and Vibratory Loads Data From a Wind-Tunnel Test of a Model Helicopter Main- Rotor Blade With a
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3165.ps.Z, 19970430 NASATechnical Paper 3165AnnoyanceCausedbyAircraftEn Route NoiseDavid A.McCurdyMarch1992 AbstractAlaboratoryexperimentwasconducted toquantifythe annoyancer esponseofpeopleontheg roundto enroutenoiseg eneratedby aircraftat cruiseconditions.Thee nroutenoises wereground-levelrecordingsofeightadvanced
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm110335.ps.Z, 19970501 NASA Technical Memorandum 110335Experimental Robot Position Sensor FaultTolerance Using Accelerometers and JointTorque SensorsHal A. Aldridge and Jer-Nan JuangLangley Research Center, Hampton, VirginiaMarch 1997National Aeronautics andSpace AdministrationLangley Research CenterHampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr201683.ps.Z, 19970501 iiiContentsSUMMARY............................................................................................................................1INTRODUCTION.....................................................................................................................3NASA s Role in Promoting
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-1isios-brb.ps.Z, 19970502 2.2 CLOUD FORCING AND THE EARTH'S RADIATION BUDGET: NEW IDEAS AND NEW OBSERVATIONS Bruce R. Barkstrom NASA Langley Research Center, Hampton, Virginia 1. NEW PERSPECTIVES ON CLOUD-RADIATIVE FORCING When the Earth Radiation Budget Experiment (ERBE) produced the first measurements of cloudradiative forcing
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr201686.ps.Z, 19970505 NASA Contractor Report 201686An Approach to the Constrained Design of Natural Laminar Flow AirfoilsBradford E. GreenThe George Washington UniversityJoint Institute for Advancement of Flight SciencesLangley Research Center, Hampton, VirginiaCooperative Agreement NCC1-24February 1997National Aeronautics
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr201680.ps.Z, 19970505 NASA Contractor Report 201680Aviation System Analysis Capability (ASAC) Quick Response System (QRS) Test ReportEileen Roberts, James A. Villani, and Paul RitterLogistics Management Institute, McLean, VirginiaContract NAS2-14361April 1997National Aeronautics andSpace AdministrationLangley Research
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm110325.ps.Z, 19970506 NASA Technical Memorandum 110325The Upper Atmosphere Research Satellite In-Flight DynamicsStanley E. WoodardLangley Research Center, Hampton, VirginiaApril 1997National Aeronautics andSpace AdministrationLangley Research CenterHampton, Virginia 23681-0001 AbstractUpper Atmosphere Research Satellite
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr201682.ps.Z, 19970506 NASA Contractor Report 201682Estimating the Effects of the Terminal Area Productivity ProgramDavid A. Lee, Peter F. Kostiuk, Robert V. Hemm, Earl R. Wingrove III, and Gerald ShapiroLogistics Management Institute, McLean, VirginiaContract NAS2-14361April 1997National Aeronautics andSpace
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr201681.ps.Z, 19970506 NASA Contractor Report 201681ASAC Executive Assistant ArchitectureDescription SummaryEileen Roberts and James A. VillaniLogistics Management Institute, McLean, VirginiaContract NAS2-14361April 1997National Aeronautics andSpace AdministrationLangley Research CenterHampton, Virginia 23681-0001
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/NASA-94-tm4539.ps.Z, 19970507 NASATechnical Memorandum 4539EM-ANIMATEAComputerProgramfor Displaying andAnimatingElectromagneticNear-Field andSurface-CurrentSolutionsKamW. HomLangley ResearchCenterfflHampton,VirginiaNationalAeronautics and Space AdministrationLangleyResearchCenterfflHampton, Virginia23681-0001May1994 Theuse of
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3226.ps.Z, 19970508 NASATechnical Paper 3226EffectofTemperatureandGapOpening Rateon theResiliencyofCandidateSolid RocketBooster O-RingMaterialsCynthia L. LachJune1992 Ab stractAsapartoftheredesign of theSpaceShuttlesolidrocketmotorfollowingtheChallen geraccident, thefie ldandnozzle-to-case jointswere designed tomin-imize
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm110331.ps.Z, 19970512 NASA Technical Memorandum 110331U. S. Army Research Laboratory Technical Report 1342Fatigue Debonding Characterization in Composite Skin/Stringer ConfigurationsMichael K. CvitkovichNational Research Council Resident Research AssociateLangley Research Center, Hampton, VirginiaT. Kevin O'BrienVehicle
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr4772.ps.Z, 19970514 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-0001NASA Contractor Report 4772The Volume Grid Manipulator (VGM): A GridReusability ToolStephen J. AlterLockheed Martin Engineering & Sciences Company Hampton, VirginiaApril 1997Prepared for Langley Research
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-53ahs-gbm.ps.Z, 19970514 FATIGUE LIFE METHODOLOGY FOR TAPERED COMPOSITE FLEXBEAM LAMINATES 1 Gretchen B. Murri T. Kevin O'Brien U.S. Army Research Laboratory Vehicle Technology Center Hampton, VA Carl Q. Rousseau Bell Helicopter Textron Ft. Worth, TX American Helicopter Society 53rd Annual Forum April 29 - May 1, 1997 Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm4756.ps.Z, 19970516 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Memorandum 4756 Evaluation of the Low-Speed Stability and Control Characteristics of a Mach 5.5 Waverider Concept David E. Hahne Langley Research Center Hampton, Virginia May 1997 Printed
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tp/NASA-97-tp3626.ps.Z, 19970516 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3626 Texture Modification of the Shuttle Landing Facility Runway at Kennedy Space Center Robert H. Daugherty and Thomas J. Yager Langley Research Center Hampton, Virginia May 1997
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr201692.ps.Z, 19970519 Analysis of Discontinuties in a Rectangular Waveguide Using Dyadic Green s Function Approach in Conjunction With Method of Moments M. D. Deshpande ViGYAN Inc., Hampton, VA. 23681 Contract NAS1-19341 April 1997 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tp/NASA-97-tp3628.ps.Z, 19970519 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3628 Static Investigation of a Multiaxis Thrust- Vectoring Nozzle With Variable Internal Contouring Ability David J. Wing, Charles T. L. Mills, and Mary L. Mason Langley Research
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-27ices.ps.Z, 19970520 97ES-29 Thermal Design and Analysis for the Cryogenic MIDAS Experiment Ruth McElroy Amundsen NASA Langley Research Center
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/aiaa/NASA-aiaa-97-1595.ps.Z, 19970527 AEROACOUSTIC MEASUREMENTS OF A WING-FLAP CONFIGURATION Kristine R. Meadows Thomas F. Brooks y William M. Humphreys z William W. Hunter x Carl H. Gerhold { Fluid Mechanics and Acoustics Division NASA Langley Research Center Hampton, VA 23681-0001
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm4760.ps.Z, 19970529 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Memorandum 4760 ARL Technical Report 1389 Rotating Shake Test and Modal Analysis of a Model Helicopter Rotor Blade W. Keats Wilkie, Paul H. Mirick, and Chester W. Langston Vehicle Technology
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tp/NASA-97-tp3661.ps.Z, 19970529 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3661 Angular Alignment Testing of Laser Mirror Mounts Under Temperature Cycling K. T. Bullock, R. J. De Young, and S. P. Sandford Langley Research Center Hampton, Virginia June 1997
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm110336.ps.Z, 19970603 NASA Technical Memorandum 110336 Vertical Tail Buffeting Alleviation Using Piezoelectric Actuators - Some Results of the Actively Controlled Response of Buffet-Affected Tails (ACROBAT) Program Robert W. Moses Langley Research Center, Hampton, Virginia April 1997 National Aeronautics and Space
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-ceas-rwm.ps.Z, 19970603 ACTIVE VERTICAL TAIL BUFFETING ALLEVIATION ON A TWIN-TAIL FIGHTER CONFIGURATION IN A WIND TUNNEL Robert W. Moses Aeroelasticity Branch NASA Langley Research Center MS 340 Hampton, VA 23681, USA email address: r.w.moses@larc.nasa.gov
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/jp/NASA-97-citmmo-glg.ps.Z, 19970603 Integrating Information Technologies Into Large Organizations Gretchen L. Gottlich John M. Meyer Michael L. Nelson NASA Langley Research Center, Hampton VA David J. Bianco Computer Sciences Corporation, Hampton VA This is a pre-print version of Chapter 17 in Cases on Information Technology Management in
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/aiaa/NASA-aiaa-97-2260.ps.Z, 19970612 AIAA 97-2260 15th AIAA Applied Aerodynamics Conference June 23 25, 1997 / Atlanta, GA PREDICTION OF HIGH-LIFT FLOWS USING TURBULENT CLOSURE MODELS Christopher L. Rumsey,a,* Thomas B. Gatski,a Susan X. Ying,b,* and Arild Bertelrudc,* aNASA Langley Research Center, Mail Stop 128, Hampton, VA 23681-0001,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tp/NASA-97-tp3656.ps.Z, 19970612 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3656 New Parameterization of Neutron Absorption Cross Sections Ram K. Tripathi Hampton University Hampton, Virginia John W. Wilson and Francis A. Cucinotta Langley Research Center
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-acc-kbl.ps.Z, 19970613 CLOSED FORM SOLUTION FOR MINIMUM NORM MODEL-VALIDATING UNCERTAINTY Kyong Been Lim Guidance & Control Branch, Flight Dynamics & Control Division NASA Langley Research Center, MS 161 Hampton, VA 23681-0001 k.b.lim@larc.nasa.gov
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/NASA-97-rp1395.ps.Z, 19970616 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-2199 NASA Reference Publication 1395 Laser-Induced Damage Threshold and Certification Procedures for Optical Materials June 1997 Printed copies available from the following: NASA Center for AeroSpace
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-6aisc-lhc.ps.Z, 19970617 5. Ramanathan, V., R. D. Cess, E. F. Harrison, P. Minnis, B. R. Barkstrom, E. Ahmad, D. Hartmann, Cloud-Radiative Forcing and Climate: Results from the Earth Radiation Budget Experiment, Science, Vol. 243, 6 January, 1989, pp. 57-63. 6. Hartmann, D. L., Radiative Effects of Clouds on Earth s Climate, in
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/aiaa/NASA-aiaa-97-2536.ps.Z, 19970617 1 American Institute of Aeronautics and Astronautics NUMERICAL STUDY OF A CONTINUUM SONIC JET INTERACTING WITH A RAREFIED FLOW by Christopher E. Glass* NASA Langley Research Center Hampton, VA 23681-0001 andGerald J. LeBeau NASA Lyndon B. Johnson Space Center Houston, TX 77058-3696 Abstract The results
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tp/NASA-97-tp3630.ps.Z, 19970623 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-2199 NASA Technical Paper 3630 Calculation of Heavy Ion Inactivation and Mutation Rates in Radial Dose Model of Track Structure Francis A. Cucinotta and John W. Wilson Langley Research Center Hampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/NASA-92-tp3171.ps.Z, 19970623 REPOR T DOCUMENTATIONPAGEForm ApprovedOMB No. 704-0188Publicreportingburdenforthiscollection of information is estimatedtoa verage1hourperresponse,includingthetimeforreviewing instructions,sear chingexistingdata sources,g atheringandmaintainingthe dataneeded,andcompletingandreviewingthe co
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tp/NASA-97-tp3633.ps.Z, 19970624 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 NASA Technical Paper 3633 Combustibility Tests of 1,1,1,2-tetrafluoroethane in a Simulated Compressor Cylinder Dale A. Babcock and Robert A. Bruce Langley Research Center Hampton, Virginia June 1997
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr201710.ps.Z, 19970626 NASA Contractor Report 201710 Analysis of Waveguide Junction Discontinuities Using Finite Element Method Manohar D. Deshpande ViGYAN, Inc., Hampton, Virginia Contract NAS1-19341 July 1997 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 1ContentsList of
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/aiaa/NASA-aiaa-97-2510.ps.Z, 19970627 Low-Density Aerodynamics of the Stardust Sample Return Capsule Richard G. Wilmoth , Robert A. Mitcheltreey, and James N. Mossz NASA Langley Research Center, Hampton, VA 23681 The aerodynamics of the Stardust Sample Return Capsule are analyzed in the lowdensity, transitional flow regime using
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-1683.ps.Z, 19970707 QUADRATURE-FREE IMPLEMENTATION OF THE DISCONTINUOUS GALERKIN METHOD FOR HYPERBOLIC EQUATIONS H. L. Atkins* NASA Langley Research Center, Hampton, VA 23681 Chi-Wang Shu Brown University, Providence, RI 02912 A discontinuous Galerkin formulation that avoids the use of discrete quadrature formulas is
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/aiaa/NASA-aiaa-97-2032.ps.Z, 19970707 Local Analysis of Shock Capturing Using Discontinuous Galerkin Methodology H. L. Atkins* NASA Langley Research Center Hampton, VA 23681-0001
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm112853.ps.Z, 19970707 NASA Technical Memorandum 112853 Predicting NonInertial Effects With Algebraic Stress Models Which Account for Dissipation Rate Anisotropies T. Jongen and L. Machiels Swiss Federal Institute of Technology, Lausanne, Switzerland T. B. Gatski Langley Research Center, Hampton, Virginia May 1997 National
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/aiaa/NASA-aiaa-97-1581.ps.Z, 19970707 Continued Development of the Discontinuous Galerkin Method for Computational Aeroacoustic Applications H. L. Atkins* NASA Langley Research Center Hampton, VA, 23681-0001
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/aiaa/NASA-aiaa-97-2074.ps.Z, 19970708 AN IMPROVED TREATMENT OF EXTERNAL BOUNDARY FOR THREE-DIMENSIONAL FLOW COMPUTATIONS Semyon V. Tsynkovy Veer N. Vatsaz NASA Langley Research Center, Hampton, VA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tp/NASA-97-tp3659.ps.Z, 19970715 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-2199 NASA Technical Paper 3659 Buckling Behavior of Long Symmetrically Laminated Plates Subjected to Shear and Linearly Varying Axial Edge Loads Michael P. Nemeth Langley Research Center Hampton, Virginia July
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-ASME-djw.ps.Z, 19970717 This paper is declared a work of the United States 1 Government and is therefore in the public domain. 1997 ASME Fluids Engineering Division Summer Meeting FEDSM 97 June 22 - 26, 1997 FEDSM97-3228 FLUIDIC THRUST VECTORING OF AN AXISYMMETRIC EXHAUST NOZZLE AT STATIC CONDITIONS David J. Wing NASA Langley
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-aps-mdd.ps.Z, 19970722 Analysis of Stub Loaded Microstrip Patch Antennas M. D. Deshpande* ViGYAN Inc., 30 Research Drive, Hampton M. C. Bailey NASA Langley Research Center, Hampton. A microstrip patch antenna fed by a coaxial probe and reactively loaded by a open circuited microstrip line has been used previously to produce
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr201679.ps.Z, 19970724 NASA Contractor Report 201679The ASAC Flight Segment and Network Cost ModelsBruce J. Kaplan, David A. Lee, Nusrat Retina, and Earl R. Wingrove IIILogistics Management Institute, McLean, VirginiaBrett Malone, Stephen G. Hall, and Scott A. HouserPhoenix Integration, Phoenix, ArizonaContract
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-ieee-aes-95p7-13.ps.Z, 19970725 IEEE AES Systems Magazine, vol. 10, no. 5, May 1995, pp. 7-13. Accessing NASA Technology with the World Wide Web Michael L. Nelson Systems Analyst, Information Systems Division, NASA Langley Research Center David J. Bianco Systems Analyst, Computer Sciences Corporation, NASA Langley Research Center
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/aiaa-95-1820.ps.Z, 19970725 INVERSE DESIGN OF NACELLES USING MULTI-BLOCK NAVIER STOKES CODES D. A. Naik ViGYAN, Inc., Hampton, Virginia 23666 S. E. Krist, R. L. Campbell, and V. N. Vatsa NASA Langley Research Center, Hampton, Virginia 23681 P. G. Buning NASA Ames Research Center, Moffett Field, California 94035 and L. M. Gea
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-isuac-cal.ps.Z, 19970728 SPASIM: A SPACECRAFT SIMULATOR Carlos A. Liceaga NASA Langley Research Center 8 Langley Blvd., M/S 328 Hampton, VA 23681-0001 c.a.liceaga@larc.nasa.gov
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/tm4602.ps.Z, 19970801 NASA Technical Memorandum 4602 Mach 10 Computational Study of a Three-Dimensional Scramjet Inlet Flow Field Scott D. Holland March 1995 NASA Technical Memorandum 4602 Mach 10 Computational Study of a Three-Dimensional Scramjet Inlet Flow Field Scott D. Holland Langley Research Center Hampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3230.ps.Z, 19970804 NASATechnical Paper 3230Inertial Oscillation of a VerticalRotating DraftWith ApplicationtoaSupercell StormRobert C.CostenandLarry V.StockSeptember1992 Contents1.Introduction................................ 12. ModelDescription ............................. 22 .1. Coordin
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm4565.ps.Z, 19970804 NASATechnical Memorandum 4565Preliminary EstimatesofNucleon Fluxes inaWater TargetExposedto Solar-Flare Protons:BRYNTRNVersus Monte Carlo CodeJudy L.Shinn,John W.Wilson, M.A.Lone,P.Y.Wong,andRobertC.CostenJune1994 AbstractAbaryontransport code(BRYNTRN)haspreviouslybeenverifiedusing available
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm112863.ps.Z, 19970807 NASA Technical Memorandum 112863 Recursive Deadbeat Controller Design Jer-Nan Juang Langley Research Center, Hampton, Virginia Minh Q. Phan Princeton University, Princeton, New Jersey May 1997 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 Recursive
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm112862.ps.Z, 19970807 NASA Technical Memorandum 112862 Deadbeat Predictive Controllers Jer-Nan Juang Langley Research Center, Hampton, Virginia Minh Phan Princeton University, Princeton, New Jersey May 1997 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 Deadbeat Predictive
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/aiaa/NASA-aiaa-97-3797.ps.Z, 19970815 Copyright 1997 by the American Institute of Aeronautics and Astronautics, Inc. No copyright is asserted in the United States under Title 17, US Code. The US Government has a royalty-free license to exercise all rights under the copyright claimed herein for Governmental Purposes. All other rights are
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/aiaa/NASA-aiaa-97-2569.ps.Z, 19970822 32nd AIAA Thermophysics Conference June 23-25, 1997 / Atlanta, GA AIAA 97-2569 Transition Effects on Heating in the Wake of a Blunt Body Brian R. Hollis, John N. PerkinsR aleigh, NC 27695N orth Carolina State University Grants NAG1-1663 and NAGW-1331 Prepared for NASA Langley Research Center Transition
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/aiaa/NASA-aiaa-97-3712.ps.Z, 19970825 f
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/aiaa/NASA-aiaa-97-3711.ps.Z, 19970825 American Institute of Aeronautics and Astronautics 1 FLIGHT TEST VALIDATION OF OPTIMAL INPUT DESIGN AND COMPARISON TO CONVENTIONAL INPUTS Eugene A. Morelli* NASA Langley Research Center Hampton, Virginia USA 23681 - 0001
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-30cfd-twr.ps.Z, 19970826 Relaxation Revisited\|A Fresh Look at Multigrid for Steady Flows Thomas W. Roberts , David Sidilkovery and R. C. Swanson 1 Introduction The year 1971 saw the publication of one of the landmark papers in computational aerodynamics, that of Murman and Cole . As with many seminal works, its significance
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/aiaa/NASA-aiaa-97-1949.ps.Z, 19970826 TEXTBOOK MULTIGRID EFFICIENCY FOR THE STEADY EULER EQUATIONS Thomas W. Roberts NASA Langley Research Center David Sidilkovery Institute for Computer Applications in Science and Engineering and R. C. Swanson NASA Langley Research Center Hampton, VA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-11iced-jlr.ps.Z, 19970827 INTERNATIONAL CONFERENCE ON ENGINEERING DESIGN ICED 97 TAMPERE, AUGUST 19 - 21, 1997 REDUCING DESIGN CYCLE TIME AND COST THROUGH PROCESS RESEQUENCING James L. Rogers Keywords: design cycle, genetic algorithm, decomposition, concurrent engineering 1 Introduction In today s competitive environment,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr201730.ps.Z, 19970902 NASA Contractor Report 201730 User s Manual for FEMOM3DS Version 1.0 C. J. Reddy Hampton University, Hampton, Virginia M. D. Deshpande ViGYAN,Inc., Hampton, Virginia NASA Cooperative Agreement NCC1-231 August 1997 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm112867.ps.Z, 19970902 NASA Technical Memorandum 112867 Aerodynamic Design on Unstructured Grids for Turbulent W. Kyle Anderson and Daryl L. Bonhaus Langley Research Center, Hampton, Virginia June 1997 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-0001 Flows 1 Introduction
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm4779.ps.Z, 19970903 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-2199 NASA Technical Memorandum 4779 ARL Technical Report 1402 Quasi-Static Viscoelasticity Loading Measurements of an Aircraft Tire Angela J. Mason and John A. Tanner Langley Research Center Hampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3183.ps.Z, 19970910 NASATechnical Paper 3183Venturi Air-JetVacuumEjectorsforHigh-VolumeAtmosphericSamplingonAircraft PlatformsGeraldF.Hill,Glen W.Sachse,DouglasC.Young, LarryO. Wade, andLewisG.BurneyMarch 1992 Theuse of trademark s or names of manufacturers inthisre portis foraccurate re portinganddoes not constitute ano
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3105.ps.Z, 19970910 NASATechnical Paper 3105Influenceof AirfoilGeometry onDeltaWingLeading-Edge Vortices and Vortex-InducedAerodynamics atSupersonicSpeedsRichardM.Wood,James E. Byrd,andGary F. WesselmannMarch 1992 ContentsSymbols................................... vA bstract................................... 1I
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3187.ps.Z, 19970910 NASATechnical Paper 3187Fault ToleranceofArtificial NeuralNetworksWith Applications in CriticalSystemsPeterW.Protzel,DanielL. Palumbo, and MichaelK.ArrasApril 1992 AbstractOneofthe keybene tsoffuture hardwareimplementationsofcertainartificialneuralnetworks (ANN's)
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3184.ps.Z, 19970910 NASATechnical Paper 3184Wind TunnelAerodynamic Characteristics of aTransport-TypeAirfoil in a SimulatedHeavyRainEnvironmentGaudyM. Bezos,R. Earl Dunham,Jr.,Garl L. Gentry,Jr., and W.Edward Melson,Jr.August 1992 SummaryAwind tu nnel investigation was conductedwi tha cambered airfoil representative
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3186.ps.Z, 19970910 NASATechnical Paper 3186DirectSimulationofHigh-SpeedMixing LayersH. S.Mukunda,B.Sekar,M. H.Carpenter, J.PhilipDrummond, andAjay KumarJuly 1992 SummaryThi s computationalstudyis anexploration ofnon reacting high-speed mixinglayers. The compu -ta tionsaremade withacodebasedon anaccuratehi gherorder
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3189.ps.Z, 19970910 NASATechnical Paper 3189Unsteady Pressure Loads ina GenericHigh-Speed EngineModelTonyL. Parrott,Michael G.Jones, andErnieM. ThurlowDecember 1992 SummaryFluctuating pressureloadswere measuredalongthe top interior wall ofageneric scramjetenginemodelduringaseriesof pe rformancetestsconduc tedin
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3196.ps.Z, 19970910 NASATechnical Paper 3196EffectofLow-SpeedImpactDamageandDamageLocationon BehaviorofCompositePanelsDawn C.JegleyMay1992 Theuse of trademark s or names of manufacturers inthisre portis foraccurate re portinganddoes not constitute ano fficial endorsement, either expressedor implied, of suchprodu ctsor
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3167.ps.Z, 19970910 NASATechnical Paper 3167A SimplifiedMethod forThermal Analysis ofaCowl Leading EdgeSubject toIntense LocalShock-Wave-InterferenceHeatingDavid M.McGowan,Charles J.Camarda, andStephenJ.ScottiMarch1992 Theuse of trademark s or names of manufacturers inthisre portis foraccurate re portinganddoes not
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3185.ps.Z, 19970910 NASATechnical Paper 3185MultipleLesionTrackStructure ModelJohn W. Wilson,FrancisA. Cucinotta,andJudyL. ShinnMarch 1992 AcknowledgmentThiswork issupported in partby theArmed Forces RadiobiologyR esearchInstituteunderDOD/AFRRIN92 6I. Ab stractAmultilesioncellkinetic model is derive d, andra diationkinetic
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3195.ps.Z, 19970910 NASATechnical Paper 3195BucklingBehavior of LongSymmetricallyLaminatedPlatesSubjected toCombinedLoadingsMichael P. NemethMay1992 Theuse of trademark s or names of manufacturers inthisre portis foraccurate re portinganddoes not constitute ano fficial endorsement, either expressedor implied, of suchprodu
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3169.ps.Z, 19970910 NASATechnical Paper 3169Diffracted andHead WavesAssociatedWithWaveson NonseparableSurfacesRaymondL.BargerMarch1992 Ab stractAtheory is presentedforcomputingwavesradiatedfrom waveson a smoothsurface. Withthe assumption that attenuationof thes urface waveisdueonly toradiation and not to dissipationin thes
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3172.ps.Z, 19970910 NASATechnical Paper 3172Comparison ofJetPlume Shape PredictionsandPlumeInfluence onSonic Boom SignatureRaymondL.BargerandN. Duane MelsonMarch 1992 Ab stractAn Euler shock- ttingmarching codeyieldsgood agreement withs emiempiricallydeterminedplumeshapes,althoughthe agreement de-cr easessomewhatwith
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3192.ps.Z, 19970910 NASATechnical Paper 3192StressConcentrationsfor Straight-ShankandCountersunkHolesinPlatesSubjected toTension, Bending,andPinLoadingK.N. Shivakumar and J. C. Newman,Jr.June1992 Ab stractAthree-dimensionalstress-concentrationanalysiswasconductedon straight-shankan d countersunk(r ivet)holesinalargeplate
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/92/tp3193.ps.Z, 19970910 NASATechnical Paper 3193The Natural FlowWing-Design ConceptRichardM.Wood andSteven X.S.BauerApril 1992 NomenclatureAcross-sectional area,in2aivariablesusedto dene airfoilgeom-etryforward ofmaximum thickness( wherei=0,1,2,or3)bwin gspan,in.CDdragcoefficient,Drag/q1SCD;cscross-sectional invisciddrag
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm4573.ps.Z, 19970912 NASATechnical Memorandum 4573AutomaticComputationofEuler-Marching andSubsonic Gridsfor Wing-FuselageConfigurationsRaymondL.Barger, MaryS.Adams, and Ramki R. KrishnanJuly 1994 NASATechnical Memorandum 4573AutomaticComputationofEuler-Marching andSubsonic Gridsfor
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-1icdns-rdj.ps.Z, 19970915 1
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm4541.ps.Z, 19970916 NASATechnical Memorandum 4541AerodynamicCharacteristicsofaPropeller-Powered High-LiftSemispan WingGarl L.Gentry, Jr.,M. A.Takallu, and ZacharyT.ApplinApril 1994 AbstractAsmall-scale semispanhigh-lift wing-flapsyste m equipped u ndert he wingwithaturbopropengineassembly was testedin the Langley1 4-
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-iongps-jlg.ps.Z, 19970926 Relative Navigation In Elliptical Orbits Using An Iterative Nonlinear Filter James L. Garrison NASA Langley Research Center, Hampton, VA Penina Axelrad University of Colorado, Boulder, CO BIOGRAPHY James Garrison is a doctoral candidate in Aerospace Engineering Sciences at the University of Colorado, he
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-23erc-jdb.ps.Z, 19970926 33.1 A COMPARISON OF INTERACTIONAL AERODYNAMICS METHODS FOR A HELICOPTER IN LOW SPEED FLIGHT John D. Berry US Army, ATCOM, AFDD Hampton, VA, USA Victor Letnikov and Irena Bavykina Mil Moscow Helicopter Plant Moscow, Russia Mark S. Chaffin Lockheed Martin Hampton, VA, USA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tp/NASA-97-tp3644.ps.Z, 19970929 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-2199 NASA Technical Paper 3644 Comparison of Stopping Power and Range Databases for Radiation Transport Study H. Tai Langley Research Center Hampton, Virginia Hans Bichsel Washington University Seattle,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/jp/NASA-97-jic-mln.ps.Z, 19971001 TRSkit: A Simple Digital Library Toolkit Michael L. Nelson Sandra L. Esler NASA Langley Research Center MS 157A Hampton, VA 23681-0001
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tp/NASA-97-tp3668.ps.Z, 19971003 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-2199 NASA Technical Paper 3668 Exposures to Solar Particle Events in Deep Space Missions John W. Wilson, Judy L. Shinn, Lisa C. Simonsen, and Francis A. Cucinotta Langley Research Center Hampton, Virginia R. R.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm4776.ps.Z, 19971003 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-2199 NASA Technical Memorandum 4776 Wrist Camera Orientation for Effective Telerobotic Orbital Replaceable Unit (ORU) Changeout Sharon Monica Jones, Hal A. Aldridge, and Sixto L. Vazquez Langley Research Center
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tp/NASA-97-tp3702.ps.Z, 19971014 September 1997NASA Technical Paper 3702Micro-Mechanical Voltage Tunable Fabry-Perot Filters Formed in (111) SiliconJames D. Patterson National Aeronautics andSpace AdministrationLangley Research CenterHampton, Virginia 23681-2199September 1997NASA Technical Paper 3702Micro-Mechanical Voltage Tunable
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-agard-dms.ps.Z, 19971017 SUMMARY This paper discusses recent applications of the ENS3DAE computational aeroelasticity method. In particular, it describes aeroelastic and unsteady aerodynamics calculations performed on wings with trailing edge control surfaces. These simulations include the investigation of control reversal for
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-ieeesmc-pcs.ps.Z, 19971017 Designing to Control Flight Crew Errors Paul C. Schutte Kelli F. Willshire NASA Langley Research Center Hampton, Virginia 23681-0001
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm4767.ps.Z, 19971021 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-2199 NASA Technical Memorandum 4767 A Feasibility Study To Control Airfoil Shape Using THUNDER Jennifer L. Pinkerton and Robert W. Moses Langley Research Center Hampton, Virginia November 1997 Printed copies
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-ieeesmc-act.ps.Z, 19971022 Pilot Performance With Predictive System Status Information Anna C. Trujillo NASA Langley Research Center Hampton, VA 23681-0001
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-81agard-jst.ps.Z, 19971022 Summary Report of the First International Symposium on Strain Gauge Balancesand Workshop on AoA/Model Deformation Measurement TechniquesJohn S. Tripp* , Ping Tcheng,Alpheus W. Burner# , and Tom D. Finley#Mail Stop 238NASA Langley Research CenterHampton, Virginia 23681USACo-Chairs of the International
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm112857.ps.Z, 19971022 September 1997NASA Technical Memorandum 112857Results of Aerothermodynamic andBoundary Layer Transition Testing of0.0362-Scale X-38 (Rev 3.1) Vehicle inNASA Langley 20-Inch Mach 6 TunnelScott A. Berry, Thomas J. Horvath, V. Eric Roback, and George B. Williams, Jr. National Aeronautics andSpace
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr4786.ps.Z, 19971022 September 1997NASA Contractor Report 4786Observed Changes in AtmosphericBoundary Layer Properties at MemphisInternational Airport During August 1995J. Allen Zak and William G. Rodgers, Jr. The NASA STI Program Office ... in ProfileSince its founding, NASA has been dedicatedto the advancement of
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm112872.ps.Z, 19971022 1IDENTIFICATION OF LINEAR AND NONLINEAR AERODYNAMIC IMPULSE RESPONSESUSING DIGITAL FILTER TECHNIQUESWalter A. SilvaAeroelasticity BranchNASA Langley Research CenterABSTRACT This paper discusses the mathematicalexistence and the numerically-correctidentification of linear and nonlinear aerodynamicimpulse
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm110340.ps.Z, 19971024 NASA Technical Memorandum 110340High Accuracy Evaluationof the Finite Fourier Transformusing Sampled DataEugene A. MorelliNASA Langley Research CenterHampton, VirginiaJune 1997National Aeronautics and Space AdministrationLangley Research CenterHampton, Virginia 23681-0001 Table of
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm112868.ps.Z, 19971024 NASA Technical Memorandum 112868Simplified Analytical Model of a Six-Degree-of-Freedom Large-Gap Magnetic Suspension SystemNelson J. GroomLangley Research Center, Hampton, VirginiaJune 1997National Aeronautics andSpace AdministrationLangley Research CenterHampton, Virginia 23681-0001
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm110303.ps.Z, 19971024 NASA Technical Memorandum 110303Damage-Tolerance Characteristics of Composite Fuselage Sandwich Structures With Thick FacesheetsDavid M. McGowan and Damodar R. AmburLangley Research Center, Hampton, VirginiaFebruary 1997National Aeronautics andSpace AdministrationLangley Research CenterHampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm112866.ps.Z, 19971024 NASA Technical Memorandum 112866Autonomous Modal Identification of the Space Shuttle Tail RudderRichard S. PappaLangley Research Center, Hampton, VirginiaGeorge H. James III and David C. ZimmermanUniversity of Houston, Houston, TexasJune 1997National Aeronautics andSpace AdministrationLangley Research
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm110272.ps.Z, 19971024 NASA Technical Memorandum 110272Cryogenic Tunnel Pressure Measurements on a Supercritical Airfoil for Several Shock Buffet ConditionsRobert E. Bartels and John W. EdwardsLangley Research Center, Hampton, VirginiaSeptember 1997National Aeronautics andSpace AdministrationLangley Research CenterHampton,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm113130.ps.Z, 19971024 September 1997NASA Technical Memorandum 113130The Effect of Spaceflight on the CriticalCurrent Density of YBa2Cu3O7-x ThickFilmsStephanie A. Wise National Aeronautics andSpace AdministrationLangley Research CenterHampton, Virginia 23681-2199September 1997NASA Technical Memorandum 113130The Effect of
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm112861.ps.Z, 19971024 NASA Technical Memorandum 112861CFL3D: Its History and Some Recent ApplicationsChristopher L. Rumsey, Robert T. Biedron, and James L. ThomasLangley Research Center, Hampton, VirginiaMay 1997National Aeronautics andSpace AdministrationLangley Research CenterHampton, Virginia 23681-0001 1CFL3D: Its
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm110341.ps.Z, 19971024 NASA Technical Memorandum 110341Offset Waveguide Transmission MeasurementsRobin L. CraveyLangley Research Center, Hampton, VirginiaMay 1997National Aeronautics andSpace AdministrationLangley Research CenterHampton, Virginia 23681-0001 1AbstractTransmission loss measurements in S-band waveguide due to
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm112856.ps.Z, 19971024 NASATechnicalMemorandum112856Reentry-FFlowfieldSolutionsat80,000ft.W.A.Wood, C.J. Riley, and F.M.CheatwoodLangleyResearchCenter,Hampton,VirginiaMay1997National Aeronautics andSpace AdministrationLangley Research CenterHampton, Virginia 23681-0001 Reentry-FFlowfieldSolutionsat80,000ft.William A.Wood
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm112852.ps.Z, 19971024 NASA Technical Memorandum 112852Research and Applications in Aeroelasticityand Structural Dynamics at the NASA Langley Research CenterIrving AbelLangley Research Center, Hampton, VirginiaMay 1997National Aeronautics andSpace AdministrationLangley Research CenterHampton, Virginia 23681-0001 RESEARCH AND
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm112858.ps.Z, 19971024 NASA Technical Memorandum 112858Comparative Results From a CFD Challenge Over a 2D Three-Element High-Lift AirfoilSteven M. KlausmeyerWichita State University, Wichita, KansasJohn C. LinLangley Research Center, Hampton, VirginiaMay 1997National Aeronautics andSpace AdministrationLangley Research
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm110344.ps.Z, 19971024 NASA Technical Memorandum 110344Complex Permittivities of Candidate Radome Materials at W-bandRobin L. CraveyLangley Research Center, Hampton, VirginiaMay 1997National Aeronautics andSpace AdministrationLangley Research CenterHampton, Virginia 23681-0001 The use of trademarks or names of manufacturers
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm112874.ps.Z, 19971024 NASA Technical Memorandum 112874Viscous Driven-Cavity SolverUser's ManualWilliam A. WoodLangley Research Center, Hampton, VirginiaSeptember 1997National Aeronautics andSpace AdministrationLangley Research CenterHampton, Virginia 23681-0001 ViscousDriven-CavitySolverUser'sManualWilliam A.Wood
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm110309.ps.Z, 19971024 NASA Technical Memorandum 110309Evaluation of a Composite Sandwich Fuselage Side Panel With Damage and Subjected to Internal PressureMarshall Rouse and Damodar R. AmburLangley Research Center, Hampton, VirginiaJerry Bodine and Bernhard DopkerBoeing Commercial Aircraft Company, Seattle,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm110343.ps.Z, 19971024 NASA Technical Memorandum 110343A Candidate Wake Vortex Strength Definition for Application to the NASA Aircraft Vortex Spacing System (AVOSS)David A. HintonLangley Research Center, Hampton, VirginiaChris R. TatnallGeorge Washington UniversityJoint Institute for Advancement of Flight SciencesLangley
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm112855.ps.Z, 19971024 NASA Technical Memorandum 112855U. S. Army Research Laboratory Technical Report 1423XV-15 Structural-Acoustic DataKaren H. LyleVehicle Technology CenterU.S. Army Research LaboratoryLangley Research Center, Hampton, VirginiaJune 1997National Aeronautics andSpace AdministrationLangley Research
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-ahs-ff.ps.Z, 19971027 SUPERSONIC QUADRUPOLE NOISE THEORY FOR HIGH-SPEED HELICOPTER ROTORS F. Farassat and Kenneth S. Brentner Senior Research Scientist Research Engineer NASA Langley Research Center Hampton, Virgina
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-esars-adl.ps.Z, 19971028 Remo te Sensing fromGeostationary Orbit: GEO TROPSAT,A NewConcept for Atmospheric Remote SensingAlan D. Littlea, Doreen O. Neila, Glen W. Sachsea, Jack Fishmana, Arlin J. KruegerbaNASA Langley Research Center, M/S 468, Hampton VA 23681-0001bNASA Goddard Space Flight CenterABSTRACTThe Geostationary T
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-4lsad-cjr.ps.Z, 19971029 Distributed-Memory Computing With the Langley Aerothermodynamic Upwind Relaxation Algorithm (LAURA) Christopher J. Riley and F. McNeil Cheatwoody NASA Langley Research Center, Hampton, VA 23681 Paper Presented at the 4th NASA National Symposium on Large-Scale Analysis and Design on High-Performance
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr206232.ps.Z, 19971030 September 1997NASA/CR-97-206232TBIEM3D - A Computer Program forPredicting Ducted Fan Engine NoiseVersion 1.1M. H. Dunn The NASA STI Program Office ... in ProfileSince its founding, NASA has been dedicatedto the advancement of aeronautics and spacescience. The NASA Scientific and TechnicalInformation
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm110204.ps.Z, 19971030 1Structural Test Documentation and Results for the McDonnellDouglas All-Composite Wing Stub BoxDawn C. JegleyandHarold G. BushAbstractThe results of a series of tests conducted at the NASA Langley Research Centerto evaluate the behavior of an all-composite full-scale wing box are presented.The wing stub
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr201753.ps.Z, 19971031 October 1997NASA Contractor Report 201753Oxidation and Emittance Studies ofCoated Mo-ReDavid E. Glass The NASA STI Program Office ... in ProfileSince its founding, NASA has been dedicatedto the advancement of aeronautics and spacescience. The NASA Scientific and TechnicalInformation (STI) Program Office
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm113131.ps.Z, 19971031 October 1997NASA Technical Memorandum 113131A Succinct Naming Convention forLengthy Hexadecimal NumbersMichael S. Grant The NASA STI Program Office ... in ProfileSince its founding, NASA has been dedicatedto the advancement of aeronautics and spacescience. The NASA Scientific and TechnicalInformation
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-48iac-wmp.ps.Z, 19971103 COMMERCIALIZATION OFTHE SPACE FRONTIERWilliam M. PilandNASA Langley Research CenterHampton, Virginia 23681-0001IAF-97-IAA.1.3.01Presented at the48th International Astronautical CongressOctober 6-10, 1997Turin, Italy
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm4787.ps.Z, 19971103 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-2199 NASA Technical Memorandum 4787 Thermal Conductivity Database of Various Structural Carbon-Carbon Composite Materials Craig W. Ohlhorst, Wallace L. Vaughn, Philip O. Ransone, and Hwa-Tsu Tsou Langley
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-ahs-khl.ps.Z, 19971104 A Comparison of Measured and Predicted XV-15 Tiltrotor Surface Acoustic PressuresKaren H. LyleAerospace Engineer, US Army Vehicle Technology CenterHampton, VACasey L. BurleyAerospace Engineer, NASA Langley Research CenterHampton, VADevon S. PrichardAerospace Engineer, Lockheed Martin Engineering and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-ahs-hej.ps.Z, 19971105 15* Note: Trailer 1 from main tip vortex and Trailer 2 from inboard tip vortex Table 1: BVI Interaction Locations And SourcesBlade MissDistance Location ofInteraction Depositedat Azimuth FromTrailer*Base 0.01R 75.0 140. 2LinT wt 0.0125R 70.0 125. 1Lamda1 0.0125R 70.0 125. 1Lamada2 0.0125R 70.0 125.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-16dasc-raw.ps.Z, 19971107 The NASA High Intensity Radiated Fields Laboratory Reuben A. Williams NASA Langley Research Center M/S 130 Hampton, Virginia 23681-0001
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tp/NASA-97-tp3671.ps.Z, 19971110 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-2199 NASA Technical Paper 3671 Measured Changes in C-Band Radar Reflectivity of Clear Air Caused by Aircraft Wake Vortices Anne I. Mackenzie Langley Research Center Hampton, Virginia November 1997 Printed
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-16dasc-cmh.ps.Z, 19971110 To appear in the Proceedings of the 16th Digital Avionics Systems Conference, October 1997 WHY ENGINEERS SHOULD CONSIDER FORMAL METHODS C. Michael Holloway NASA Langley Research Center Mail Stop 130 / 1 South Wright Street Hampton, Virginia 23681-0001 E-mail: c.m.holloway@larc.nasa.gov
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tp/NASA-97-tp3672.ps.Z, 19971110 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-2199 NASA Technical Paper 3672 Application of Wind Tunnel Free-Flight Technique for Wake Vortex Encounters Jay M. Brandon, Frank L. Jordan, Jr., and Robert A. Stuever Langley Research Center Hampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tp/NASA-97-tp206234.ps.Z, 19971114 NASA/TP-97-206234Development of Stitched, Braided andWoven Composite Structures in the ACTProgram and at Langley Research Center(1985 to 1997)Summary and BibliographyMarvin B. Dow and H. Benson DexterNovember 1997 The NASA STI Program Office . . . in ProfileSince its founding, NASA has been dedicatedto
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/aiaa/NASA-aiaa-97-2698.ps.Z, 19971117 American Institute of Aeronautics and Astronautics1DETERMINING FUNCTIONAL RELIABILITY OF PYROTECHNIC MECHANICAL DEVICESLaurence J. Bement*NASA Langley Research CenterHampton, VirginiaHerbert A. MulthaupNew England, North DakotaABSTRACTThis paper describes anew approach forevaluating mechanical
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/aiaa/NASA-aiaa-97-0231.ps.Z, 19971117 Satellite Systems Design/Simulation Environment: A Systems Approach to Pre-Phase A DesignMelvin J. Ferebee, Jr., Patrick A. Troutman, Donald W. Monell NASA Langley Research Center, Hampton, Virginia AIAA Paper No. 97-0231 34th AIAA Aerospace Sciences Meeting and Exhibit January 6-9, 1997, Reno, Nevada
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr201720.ps.Z, 19971117 NASA Contractor Report 201720W-band Free Space Permittivity Measurement Setup for Candidate Radome MaterialsDion T. FralickLockheed Martin Engineering & Sciences, Hampton, VirginiaContract NAS1-96014August 1997National Aeronautics andSpace AdministrationLangley Research CenterHampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tp/NASA-97-tp3637.ps.Z, 19971117 National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681-2199 NASA Technical Paper 3637 Guide to AERO2S and WINGDES Computer Codes for Prediction and Minimization of Drag Due to Lift Harry W. Carlson Lockheed Martin Engineering & Sciences Hampton, Virginia Julio Chu
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/jp/NASA-97-joa-jcl.ps.Z, 19971117 1PARAMETRIC INVESTIGATION OF A HIGH-LIFT AIRFOILAT HIGH REYNOLDS NUMBERSJohn C. Lin*NASA Langley Research Center, Hampton, VA 23681-0001andChet J. Dominik McDonnell Douglas Aerospace, Long Beach, CA 90810-1870AbstractA new two-dimensional, three-element, advanced high-lift research airfoil has been
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/aiaa/NASA-aiaa-97-2110.ps.Z, 19971117 APPLICATION FRONTIERS OF DESIGNER FLUID MECHANICS --VISIONS VERSUS REALITYORAN ATTEMPT TO ANSWER THE PERENNIAL QUESTION WHY ISN T IT USED Dennis M. Bushnell*Chief ScientistNASA - Langley Research CenterHampton, Virginia 23681-0001ABSTRACTAny new concept must successfully transit twosequential filters
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr201687.ps.Z, 19971117 NASA Contractor Report 201687Spin-Tunnel Investigation of a 1/28-Scale Model of the NASA F-18 High Alpha Research Vehicle (HARV) With and Without Vertical TailsC. Michael FremauxLockheed Martin Engineering & Sciences Company, Hampton, VirginiaContract NAS1-19000April 1997National Aeronautics andSpace
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr201701.ps.Z, 19971117 NASA Contractor Report 201701PIV Data Validation Software PackageJames L. BlackshireViGYAN, Inc., Hampton, VirginiaCONTRACT NAS1-19505June 1997National Aeronautics andSpace AdministrationLangley Research CenterHampton, Virginia 23681-0001 iPIV Data Validation Software PackageAbstractA PIV data
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr201722.ps.Z, 19971117 NASA Contractor Report 201722Asynchronous Communication of TLNS3DMB Boundary ExchangeDana P. HammondComputer Sciences Corporation, Hampton, VirginiaContract NAS1-20431June 1997National Aeronautics andSpace AdministrationLangley Research CenterHampton, Virginia 23681-0001 1AbstractThis paper describes
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/aiaa/NASA-aiaa-97-2473.ps.Z, 19971117 ComputationalAerothermodynamicDesignIssuesforHyp ersonicVehiclesPeterA.Gnoffo, K.James Weilmuenster,H. Harris Hamilton, II NASALangleyResearchCenterHampton, VA23681-0001David R. OlynickyEthira j VenkatapathyzNASAAmes ResearchCenterThermosciencesInstituteMoffettField, CA94035-1000NASAAmes
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr201734.ps.Z, 19971117 NASA Contractor Report 201734Bonding and Sealing Evaluations for Cryogenic TanksDavid E. GlassAnalytical Services & Materials, Inc., Hampton, VirginiaContract NAS1-96014August 1997National Aeronautics andSpace AdministrationLangley Research CenterHampton, Virginia 23681-0001 The use of trademarks or
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr201729.ps.Z, 19971117 NASA Contractor Report 201729Analyzing Tabular and State-Transition Requirements Specifications in PVSSam Owre, John Rushby, and Natarajan ShankarSRI International, Menlo Park, CaliforniaContract NAS1-20334July 1997National Aeronautics andSpace AdministrationLangley Research CenterHampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr201733.ps.Z, 19971117 NASA Contractor Report 201733Reflective Coating on Fibrous Insulation for Reduced Heat TransferDerek D. Hass, B. Durga Prasad, David E. Glass, and Karl E. WiedemannAnalytical Services & Materials, Inc., Hampton, VirginiaContract NAS1-19708August 1997National Aeronautics andSpace AdministrationLangley
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr4781.ps.Z, 19971117 NASA Contractor Report 4781The Joint Damping Experiment (JDX)Steven L. Folkman, Jeff G. Bingham, Jess R. Crookston, Joseph D. Dutson, Brook D. Ferney,Greg D. Ferney, and Edwin A. RowsellJune 1997Contract NAS1-19418Prepared for Langley Research Center National Aeronautics and Space AdministrationLangley
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-43iis-fjc.ps.Z, 19971118 Application of Least-Squares Adjustment Technique to GeometricCamera Calibration and Photogrammetric Flow VisualizationFang-Jenq ChenSenior Research EngineerNASA Langley Research CenterHampton, Virginia 23681-0001KEYWORDSFlow Visualization, Photogrammetry, Camera Calibration, Image ProcessingSubmitted
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-agu-rcc.ps.Z, 19971118 Tornadic Vortex Signature (TVS) Produced by ConstrainedPulsing Inertial Oscillation (PIO) ModelR. C. CostenM.S. 226, NASA Langley Research Center, Hampton, VA 23681-0001Phone: 757-864-1413; Fax: 757-864-8312E-mail: r.c.costen@larc.nasa.govAbstract.The TVS on Doppler radar indicates a midtropospheric
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-11ssdc-mrw.ps.Z, 19971118 Presented at the Eleventh Symposium on Structural Dynamics and ControlVirginia Polytechnic Institute and State Univerisy, Blacksburg, Virginia May 12-14, 1997Robust Multivariable Flutter Suppression for the Benchmark Active ControlTechnology (BACT) Wind-Tunnel ModelMartin R. WaszakNASA Langley Research
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-mtsiv-ljb.ps.Z, 19971118 An Investigation to Improve Quality Evaluations of Primers andPropellant for 20mm MunitionsL. J. BementC. HolmesJ. McGroryM. L. SchimmelPresented at theMunitions Technology Symposium IVFebruary 10-12, 1997Reno, Nevada 1SUMMARYTo reduce the frequency of electrically initiated, 20mm munition hangfires
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-53ahs-jdb.ps.Z, 19971118 1Rotor-Fuselage Interaction:Analysis and Validation with ExperimentJohn BerryAeroflightdynamics Directorate, US Army ATCOMLangley Research Center, VirginiaNicolas BettschartONERA Office National D tude et de Recherches A rospatialesCh tillon, FranceABSTRACT1The problem of rotor-fuselageaerodynamic
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/aiaa/NASA-aiaa-97-3812.ps.Z, 19971118 For permission to copy or republish, contact the American Institue of Aeronautics and Astronautics1801 Alexander Bell Drive, Suite 500, Reston, VA 20191-4344AIAA 97-3812Entry Dispersion Analysisfor the Stardust CometSample Return CapsulePrasun N. DesaiRobert A. MitcheltreeF. McNeil CheatwoodNASA Langley
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-ceas-mwn.ps.Z, 19971118 HIGHER HARMONIC CONTROL FOR TILTROTOR VIBRATION REDUCTIONMark W. NixonU.S. Army Vehicle Technology CenterNASA Langley Research Center, MS 340Hampton, Virginia 23681-0001email address: m.w.nixon@larc.nasa.govRaymond G. KvaternikNASA Langley Research Center, MS 340Hampton, Virginia 23681-0001email
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-32ailc-wdm.ps.Z, 19971119 1 ESTIMATING LOGISTICS SUPPORT OF REUSABLE LAUNCH VEHICLES DURING CONCEPTUAL DESIGN W. D. Morris, N. H. White, W. T. Davis NASA Langley Research Center Dr. C. E. Ebeling University of Dayton Paper for the 32nd Annual International Logistics Conference and Exposition August 5-7, 1997
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm206252.ps.Z, 19971120 November 1997NASA/TM-97-206252BACT Simulation User Guide(Version 7.0)Martin R. Waszak The NASA STI Program Office ... in ProfileSince its founding, NASA has been dedicatedto the advancement of aeronautics and spacescience. The NASA Scientific and TechnicalInformation (STI) Program Office plays a keypart
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm4784.ps.Z, 19971120 NASA Technical Memorandum 4784An Experimental Study of Fatigue CrackGrowth in Aluminum Sheet Subjected toCombined Bending and Membrane StressesEdward P. PhillipsOctober 1997 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-2199NASA Technical Memorandum 4784An
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tp/NASA-97-tp3658.ps.Z, 19971120 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-2199NASA Technical Paper 3658Some Solutions for the Large Deflections ofUniformly Loaded Circular MembranesW. B. FichterLangley Research Center Hampton, VirginiaJuly 1997 Printed copies available from the
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tp/NASA-97-tp3662.ps.Z, 19971120 NASA Technical Paper 3662Radiation Analysis for the Human LunarReturn MissionJ. W. Wilson, L. C. Simonsen, J. L. Shinn, R. R. Dubey, W. Jordan, and M. KimSeptember 1997 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-2199NASA Technical Paper 3662Radiation
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tp/NASA-97-tp3641.ps.Z, 19971120 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-0001NASA Technical Paper 3641ARL Technical Report 1279Stiffness Characteristics of Composite RotorBlades With Elastic CouplingsDavid J. PiatakLangley Research Center Hampton, VirginiaMark W. NixonVehicle
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tp/NASA-97-tp3631.ps.Z, 19971120 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-2199NASA Technical Paper 3631Multistage Schemes With Multigrid for Eulerand Navier-Stokes EquationsComponents and AnalysisR. C. SwansonLangley Research Center Hampton, VirginiaEli TurkelTel-Aviv University
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tp/NASA-97-tp3622.ps.Z, 19971120 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-0001NASA Technical Paper 3622State-Space System Realization With Input- andOutput-Data CorrelationJer-Nan JuangLangley Research Center Hampton, VirginiaApril 1997 Printed copies available from the following:NASA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-4isfsi-jsc.ps.Z, 19971124 COMPUTATION OF VORTEX SHEDDING AND RADIATED SOUND FOR A CIRCULAR CYLINDER Jared S. Cox Christopher L. Rumsey The George Washington University, JIAFS NASA Langley Research Center Hampton, Virginia Hampton, Virginia Kenneth S. Brentner Bassam A. Younis NASA Langley Research Center City University Hampton,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-igars-sm.ps.Z, 19971126 Asymmetry in the Diurnal Variation of Surface AlbedoS. Mayor, W. L. Smith, Jr., L. Nguyen, T. A. AlbertaAnalytical Services and Materials, Inc.One Enterprise Parkway, Suite 300Hampton, VA 23666P. Minnis, C. H. Whitlock, G. L. SchusterMS 420, NASA Langley Research CenterHampton, VA 23681-0001S. Mayor:
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm206255.ps.Z, 19971201 November 1997NASA/TM-97-206255Internal Performance of a Fixed-ShroudNonaxisymmetric Nozzle Equipped withan Aft-Hood Exhaust DeflectorScott C. Asbury The NASA STI Program Office ... in ProfileSince its founding, NASA has been dedicatedto the advancement of aeronautics and spacescience. The NASA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm113137.ps.Z, 19971202 November 1997NASA Technical Memorandum 113137Near Field Pressure Fluctuations in theExit Plane of a Choked AxisymmetricNozzleMichael K. Ponton, John M. Seiner, and Martha C. Brown The NASA STI Program Office ... in ProfileSince its founding, NASA has been dedicatedto the advancement of aeronautics and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-24nde-eim.ps.Z, 19971203 1 ULTRASONIC STUDIES OF COMPOSITES UNDERGOING THERMAL AND FATIGUE LOADING Eric I. Madaras, William P. Winfree, Patrick H. Johnston NASA Langley Research Center MS 231 Hampton, VA 23681-0001 INTRODUCTION New composite materials possess attractive properties for use in advanced aircraft. A necessary
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm112876.ps.Z, 19971204 NASA Technical Memorandum 112876Building Multi-Discipline,Multi-Format Digital Libraries UsingClusters and BucketsMichael L. NelsonLangley Research Center, Hampton, VirginiaAugust 1997National Aeronautics andSpace AdministrationLangley Research Center Hampton, Virginia 23681-0001 iBUILDING
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm112877.ps.Z, 19971204 NASA Technical Memorandum 112877Buckets, Clusters and DienstMichael L. NelsonLangley Research Center, Hampton, VirginiaKurt Maly and Stewart N. T. ShenOld Dominion University, Norfolk, VirginiaJuly 1997National Aeronautics andSpace AdministrationLangley Research CenterHampton, Virginia 23681-0001
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr206261.ps.Z, 19971204 December 1997NASA/CR-97-206261Application of AWE Along with aCombined FEM/MoM Technique toCompute RCS of a Cavity-BackedAperture in an Infinite Ground Plane Overa Frequency RangeC. J. ReddyHampton University, Hampton, VirginiaM. D. DeshpandeViGYAN, Inc., Hampton, Virginia The NASA STI Program Office ...
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm206262.ps.Z, 19971205 December 1997NASA/TM-97-206262Independent Analysis of the SpaceStation Node Modal Test DataRichard S. Pappa The NASA STI Program Office ... in ProfileSince its founding, NASA has been dedicatedto the advancement of aeronautics and spacescience. The NASA Scientific and TechnicalInformation (STI) Program
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tp/NASA-97-tp3651.ps.Z, 19971208 NASA Technical Paper 3651ATCOM Technical Report 97-A-005Full-Potential Modeling of Blade-VortexInteractionsHenry E. JonesDecember 1997 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-2199NASA Technical Paper 3651ATCOM Technical Report 97-A-005Full-Potential
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tp/NASA-97-tp3484.ps.Z, 19971209 NASA Technical Paper 3484Comparison of Several Numerical Methods forSimulation of Compressible Shear LayersChristopher A. Kennedy and Mark H. CarpenterDecember 1997 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-2199NASA Technical Paper 3484Comparison of
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-134asa-ksb.ps.Z, 19971209 NASA Langley Research Center, Hampton, VA K. S. Brentner 1 A SUPERIOR KIRCHHOFF METHOD FOR AEROACOUSTIC NOISE PREDICTION: The Ffowcs Williams Hawkings equation Kenneth S. Brentner NASA Langley Research Center Presented at the 134th Meeting of the Acoustical Society of America, San Diego, CA, December
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-3444.ps.Z, 19971210 This paper is declared a work of the U.S. Government and is not subject to copyright protection in the United States.FREE-FLIGHT INVESTIGATION OF FOREBODY BLOWINGFOR STABILITY AND CONTROLJay M. Brandon*NASA Langley Research CenterHampton, VA 23681-0001James M. Simon WL/FIGCWPAFB, OH 45433-7531D. Bruce
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr201728.ps.Z, 19971211 November 1997NASA Contractor Report 201728Translaminar Fracture Toughness of aComposite Wing Skin Made of StitchedWarp-knit FabricJohn E. Masters The NASA STI Program Office ... in ProfileSince its founding, NASA has been dedicatedto the advancement of aeronautics and spacescience. The NASA Scientific
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm112871.ps.Z, 19971215 NASA Technical Memorandum 112871Lyceum: A Multi-Protocol DigitalLibrary GatewayMing-Hokng MaaMassachusetts Institute of Technology, Cambridge, MassachusettsSandra L. EslerUniversity of Alabama, Tuscaloosa, AlabamaMichael L. NelsonLangley Research Center, Hampton, VirginiaJuly 1997National Aeronautics
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm206266.ps.Z, 19971215 NASA/TM{97{206266HypersonicPitching-MomentShiftforStardustReentryCapsuleForeb odyWil liamA.WoodLangleyResearchCenter,Hampton,VirginiaOctob er1997 TheNASASTIProgramOffice ... inProfileSince its founding, NASA has been dedicatedto the advancement of aeronautics and spacescience.The NASA Scientific and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/NASA-97-rp1404.ps.Z, 19971215 December 1997NASA Reference Publication 1404Surface-Based Observations of ContrailOccurrence Over the U.S., April 1993 -April 1994Patrick Minnis, J. Kirk Ayers, and Steven P. Weaver National Aeronautics andSpace AdministrationLangley Research CenterHampton, Virginia 23681-2199December 1997NASA Reference
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tp3447.ps.Z, 19971216 NASATechnical Paper 3447ComputerCode forDeterminationofThermallyPerfectGasPropertiesDavid W.Witteand Kenneth E. TatumSeptember1994 NASATechnical Paper 3447ComputerCode forDeterminationofThermallyPerfectGasPropertiesDavid W.WitteLangley ResearchCenterfflHampton,VirginiaKenneth
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-aiaa-96-1724.ps.Z, 19971216 American Institute of Aeronautics and Astronautics1PERFORMANCE OF OPTIMIZED ACTUATOR AND SENSORARRAYS IN AN ACTIVE NOISE CONTROL SYSTEMD. L. Palumbo and S. L. PadulaNASA Langley Research Center, Hampton, VAK. H. Lyle and J. H. ClineU. S. Army Vehicle Structures Directorate-ARL, Hampton, VAR. H.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm206271.ps.Z, 19971216 NASA/TM{97{206271 Equivalence of Fluctuation Splitting and Finite Volume for One-Dimensional Gas Dynamics William A. Wood Langley Research Center, Hampton, Virginia October 1997 The NASA STI Program Office ... in Profile Since its founding, NASA has been dedicated to the advancement of aeronautics and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tp/NASA-97-tp3682.ps.Z, 19971217 NASA Technical Paper 3682Galactic and Solar Cosmic Ray Shielding inDeep SpaceJohn W. Wilson, Francis A. Cucinotta, H. Tai, Lisa C. Simonsen, Judy L. Shinn, Shelia A. Thibeault,and M. Y. KimDecember 1997 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-2199NASA
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm206265.ps.Z, 19971217 December 1997NASA/TM-97-206265Time Evolution of Modeled ReynoldsStresses in Planar Homogeneous FlowsT. JongenSwiss Federal Institute of Technology, Lausanne, SwitzerlandT. B. GatskiLangley Research Center, Hampton, Virginia The NASA STI Program Office ... in ProfileSince its founding, NASA has been
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-tm110306.ps.Z, 19971217 NASA Technical Memorandum 110306Lateral-Directional EigenvectorFlying Qualities Guidelines forHigh Performance AircraftJohn B. DavidsonNASA Langley Research Center, Hampton, VirginiaDominick Andrisani, IIPurdue University, West Lafayette, IndianaDecember 1996National Aeronautics andSpace
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tp/NASA-97-tp3686.ps.Z, 19971218 NASA Technical Paper 3686Efficient Parallel Algorithm for DirectNumerical Simulation of Turbulent FlowsStuti Moitra and Thomas B. GatskiDecember 1997 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-2199NASA Technical Paper 3686Efficient Parallel Algorithm for
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr206263.ps.Z, 19971218 December 1997NASA/CR-97-206263Honeycomb Core Permeability UnderMechanical LoadsDavid E. Glass, V. V. Raman, Venki S. Venkat, and Sankara N. SankaranAnalytical Services and Materials, Inc., Hampton, VA The NASA STI Program Office ... in ProfileSince its founding, NASA has been dedicatedto the advancement
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tp/NASA-97-tp3669.ps.Z, 19971218 NASA Technical Paper 3669Cavity Unsteady-Pressure Measurements atSubsonic and Transonic SpeedsMaureen B. Tracy and E. B. PlentovichDecember 1997 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia 23681-2199NASA Technical Paper 3669Cavity Unsteady-Pressure Measurements
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tp/NASA-97-tp3673.ps.Z, 19971219 NASA Technical Paper 3673Invariance of Hypersonic Normal ForceCoefficients With Reynolds Number andDetermination of Inviscid Wave Drag FromLaminar Experimental ResultsJim A. Penland and Richard HawkinsDecember 1997 National Aeronautics and Space AdministrationLangley Research Center Hampton, Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm206272.ps.Z, 19971222 December 1997NASA/TM-97-206272International Space Station (ISS)Accommodation of a Single U.S.Assured Crew Return Vehicle (ACRV)Daniel D. Mazanek, Michelle A. Garn, and Patrick A. TroutmanLangley Research Center, Hampton, VAYuan Wang, Renjith R. Kumar, and Michael L. HeckAnalytical Mechanics Associates,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr206260.ps.Z, 19971230 December 1997NASA/CR-97-206260Three-Centimeter Doppler RadarObservations of Wingtip-Generated WakeVortices in Clear AirRobert E. Marshall, Ashok Mudukutore, Vicki L. H. Wissel, and Theodore Myers The NASA STI Program Office ... in ProfileSince its founding, NASA has been dedicatedto the advancement of
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr206259.ps.Z, 19971230 December 1997NASA/CR-97-206259Radar Reflectivity in Wingtip-GeneratedWake VorticesRobert E. Marshall, Ashok Mudukutore, and Vicki L. H. Wissel The NASA STI Program Office ... in ProfileSince its founding, NASA has been dedicatedto the advancement of aeronautics and spacescience. The NASA Scientific and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/jp/NASA-98-jasis-sle.ps.Z, 19971230 1 Evolution of Scientific and Technical Information Distribution Sandra L. Esler, Michael L. Nelson NASA Langley Research Center, MS 124, Hampton VA, 23681-0001. E-mail: m.l.nelson@larc.nasa.gov World Wide Web (WWW) and related information technologies are transforming the distribution of scientific and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3300.ps.Z, 19980105 NASATechnicalPaper3300February1993Mars Surface RadiationExposure forSolarMaximumConditionsand1989 SolarProton EventsLisaC. SimonsenandJohn E.Nealy NASATechnicalPaper33001993Mars Surface RadiationExposure forSolarMaximumConditionsand1989 SolarProton EventsLisaC. SimonsenandJohn
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3335.ps.Z, 19980105 NASATechnicalPaper3335April1993AnalysisoftheStagingManeuverandBoosterGlidebackGuidance foraTwo-Stage,Winged, FullyReusable LaunchVehicleJ.ChristopherNaftelandRichardW. Powell NASATechnicalPaper33351993AnalysisoftheStagingManeuverandBoosterGlidebackGuidance foraTwo-Stage,Winged, FullyReusable
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm206276.ps.Z, 19980105 December 1997NASA/TM-97-206276Analysis of Wind Tunnel LongitudinalStatic and Oscillatory Data of the F-16XLAircraftVladislav Klein, Patrick C. Murphy, Timothy J. Curry, and Jay M. Brandon The NASA STI Program Office ... in ProfileSince its founding, NASA has been dedicatedto the advancement of
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/aiaa/NASA-aiaa-98-0519.ps.Z, 19980106 1American Institute of Aeronautics and AstronauticsAIAA-98-0519SPATIAL CHARACTERISTICS OF THE UNSTEADY DIFFERENTIAL PRESSURESON 16% F/A-18 VERTICAL TAILSRobert W. Moses, Ph.D.AIAA MemberAeroelasticity BranchNASA Langley Research CenterHampton, VAHolt Ashley, Professor EmeritusAIAA Honorary
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/aiaa-93-0912.ps.Z, 19980107 AIAA 93 0192ACOMPARISONOFTHEPREDICTIVE CAPABILITIESOF SEVERAL TURBULENCEMODELS USINGUPWINDAND CENTRAL-DIFFERENCECOMPUTER CODESChristopher L. RumseyandVeerN.VatsaNASALangleyResearch CenterHampton, Virginia 23681 0001ABSTRACTFourturbulencemodelsare describedandevaluatedfor transonicflowsusingtheupwind
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/cr4492.ps.Z, 19980107 Modeling the Transition RegionBart A. SingerHigh Technology Corporation Research ScientistMail Stop 156, NASA Langley Research CenterHampton, VA 23681 Contents1Intro duction52The Domain of Dependence{FlowFeatures That Affect Tran-sition152.1Pressure Gradients::
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/cr191425.ps.Z, 19980107 A Comparison of Using APPL and PVM foraParallel Implementation of an UnstructuredGrid Generation Program T. ArthuryM. BockeliezDecemb er 28, 1992AbstractIn this report we describe our efforts to paral lelize the VGRIDSG unstructured sur-face grid generation program. The inherent paral lel nature of the
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4439.ps.Z, 19980107 NASATechnicalMemorandum4439SubsonicAerodynamicCharacteristicsof aProposedAdvancedMannedLaunchSystem Orbiter ConfigurationGeorge M.WareandCharlesH.Fox, Jr.FEBRUARY 1993 NASATechnicalMemorandum4439SubsonicAerodynamicCharacteristicsof aProposedAdvancedMannedLaunchSystem Orbiter ConfigurationGeorge
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/conf-3-ldef-wilson.ps.Z, 19980107 1LONG DURATION EXPOSURE FACILITY (LDEF) ARCHIVE SYSTEMBrenda K. WilsonBoeing Aerospace Operations, Inc.3221 N. Armistead Avenue, Suite BHampton, VA 23666-1311ph 804-766-8976 / fax 804-766-8977 / e-mail b.k.wilson@larc.nasa.govSUMMARYThe Long Duration Exposure Facility (LDEF) Archive System is designed
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3255.ps.Z, 19980107 NASATechnicalPaper3255February1993ManualFlyingof CurvedPrecision Approaches toLandingWithElectromechanicalInstrumentationAPiloted SimulationStudyCharlesE.Knox NASATechnicalPaper32551993ManualFlyingof CurvedPrecision Approaches toLandingWithElectromechanicalInstrumentationAPiloted
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3317.ps.Z, 19980108 NASATechnicalPaper3317May1993ExactMethodsforModalTransientResponse AnalysisIncluding FeedbackControlMelvin S. AndersonandW. Keith Belvin NASATechnicalPaper33171993ExactMethodsforModalTransientResponse AnalysisIncluding FeedbackControlMelvin S. AndersonOldDominionUniversityNorfolk,VirginiaW. Keith
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3310.ps.Z, 19980108 NASATechnicalPaper3310May1993HZEFRG1:An Energy-DependentSemiempiricalNuclearFragmentationModelLawrence W.Townsend,John W.Wilson,Ram K.Tripathi,John W.Norbury,Francis F.Badavi,andFerdousKhan NASATechnicalPaper33101993HZEFRG1:An Energy-DependentSemiempiricalNuclearFragmentationModelLawrence
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3312.ps.Z, 19980108 NASATechnicalPaper3312August1993Effects of RadiobiologicalUncertaintyon VehicleandHabitatShieldDesignforMissionsto the Moon and MarsJohn W.Wilson,John E.Nealy,Walter Schimmerling,Francis A.Cucinotta,andJamesS. Wood NASATechnicalPaper33121993Effects of RadiobiologicalUncertaintyon
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3331.ps.Z, 19980108 NASATechnicalPaper3331September1993Effects of WindowSizeandShape onAccuracy of SubpixelCentroidEstimationofTarget ImagesSharon S.Welch NASATechnicalPaper33311993Effects of WindowSizeandShape onAccuracy of SubpixelCentroidEstimationofTarget ImagesSharon S.WelchLangleyResearchCenterHampton,Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3311.ps.Z, 19980108 NASATechnicalPaper3311March1993Green's FunctionMethodsin HeavyIonShieldingJohn W.Wilson,RobertC. Costen,Judy L.Shinn,andFrancisF.Badavi NASATechnicalPaper33111993Green's FunctionMethodsin HeavyIonShieldingJohn W.Wilson,RobertC. Costen,and Judy L.ShinnLangleyResearchCenterHampton,VirginiaFrancis
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3323.ps.Z, 19980108 NASATechnicalPaper3323June 1993PerformanceAnalysis ofa Large-GrainDataflowSchedulingParadigmStevenD.YoungandRobert W.Wills NASATechnicalPaper33231993PerformanceAnalysis ofa Large-GrainDataflowSchedulingParadigmStevenD.YoungandRobert W.WillsLangleyResearchCenterHampton,Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr206264.ps.Z, 19980108 NASA/CR-97-206264
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3263.ps.Z, 19980108 NASATechnicalPaper3263EffectofBow-TypeInitialImperfectionOnReliabilityofMinimum-Weight StiffenedStructuralPanels NASATechnicalPaper3263EffectofBow-TypeInitialImperfectionOnReliabilityofMinimum-Weight StiffenedStructuralPanelsW.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3285.ps.Z, 19980108 NASATechnicalPaper3285April1993Description ofAlpha-NucleusInteraction Cross Sections forCosmic RayShielding StudiesFrancis A.Cucinotta,Lawrence W.Townsend,andJohn W.Wilson NASATechnicalPaper32851993Description ofAlpha-NucleusInteraction Cross Sections forCosmic RayShielding StudiesFrancis
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3241.ps.Z, 19980108 NASATechnicalPaper3241February1993AnalyticalandExperimentalInvestigation of FlutterSuppressionby PiezoelectricActuationJenniferHeeg NASATechnicalPaper32411993AnalyticalandExperimentalInvestigation of FlutterSuppressionby PiezoelectricActuationJenniferHeegLangleyResearchCenterHampton,Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3259.ps.Z, 19980108 NASATechnicalPaper3259March1993Conical Euler AnalysisandActiveRollSuppressionfor UnsteadyVorticalFlowsAboutRolling Delta WingsElizabeth M.Lee-RauschandJohn T.Batina NASATechnicalPaper32591993Conical Euler AnalysisandActiveRollSuppressionfor UnsteadyVorticalFlowsAboutRolling Delta WingsElizabeth
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3324.ps.Z, 19980108 NASATechnicalPaper3324July1993GeometricModelFromMicroscopic TheoryforNuclearAbsorptionSarahJohn,Lawrence W.Townsend,John W.Wilson,andRam K.Tripathi NASATechnicalPaper33241993GeometricModelFromMicroscopic TheoryforNuclearAbsorptionSarahJohnViGYAN, Inc.Hampton,VirginiaLawrence W.TownsendandJohn
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3302.ps.Z, 19980108 NASATechnicalPaper3302February1993Longitudinal-ControlDesignApproachforHigh-Angle-of-AttackAircraftAaronJ.OstroffandMelissaS.Proffitt NASATechnicalPaper33021993Longitudinal-ControlDesignApproachforHigh-Angle-of-AttackAircraftAaronJ.OstroffLangleyResearchCenterHampton,VirginiaMelissaS.ProffittLockheed
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3325.ps.Z, 19980108 NASATechnicalPaper3325May1993Robust Controller Designfor Flexible StructuresUsingNormalized CoprimeFactorPlantDescriptionsErnestS. Armstrong NASATechnicalPaper33251993Robust Controller Designfor Flexible StructuresUsingNormalized CoprimeFactorPlantDescriptionsErnestS.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3313.ps.Z, 19980108 NASATechnicalPaper3313May1993PerformanceCharacteristicsofTwo MultiaxisThrust-Vectoring Nozzles atMachNumbers upto 1.28DavidJ.WingandFrancisJ.Capone NASATechnicalPaper33131993PerformanceCharacteristicsofTwo MultiaxisThrust-Vectoring Nozzles atMachNumbers upto
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3283.ps.Z, 19980108 REPORT DOCUMENTATIONPAGEFormApprovedOMB No. 0704-0188Publicreportingburdenforthiscollection of information is estimatedtoaverage 1hourperresponse,includingthetimeforreviewing instructions, searchingexisting data sources,gatheringandmaintainingthedataneeded,andcompletingandreviewingthe
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3333.ps.Z, 19980108 NASATechnicalPaper3333June 1993EffectofPylon Cross-SectionalGeometries onPropulsionIntegration foraLow-WingTransportAnthonyM.Ingraldi,Dinesh A.Naik,andOdis C.Pendergraft,Jr. NASATechnicalPaper33331993EffectofPylon Cross-SectionalGeometries onPropulsionIntegration
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3268.ps.Z, 19980108 NASATechnicalPaper3268CECOMTechnicalReport92-B-014January1993Trade-OffsArisingFromMixtureofColorCueingandMonocular, Binoptic,andStereoscopicCueingInformationfor SimulatedRotorcraftFlightRussell V.ParrishandSteven P.Williams
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3301.ps.Z, 19980108 NASATechnicalPaper3301July1993AutomaticSpecificationofReliabilityModelsforFault-TolerantComputersCarlosA. Liceaga andDanielP. Siewiorek NASATechnicalPaper33011993AutomaticSpecificationofReliabilityModelsforFault-TolerantComputersCarlosA. LiceagaLangleyResearchCenterHampton,VirginiaDanielP.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3258.ps.Z, 19980108 NASATechnicalPaper3258February1993Wind-Tunnel Free-FlightInvestigation of a SupersonicPersistence FighterDavidE.Hahne,ThomasR.Wendel,andJoseph R.Boland NASATechnicalPaper32581993Wind-Tunnel Free-FlightInvestigation of a SupersonicPersistence
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3334.ps.Z, 19980108 NASATechnicalPaper3334September1993WallInterference andBoundarySimulationinaTransonicWind TunnelWith a Discretely SlottedTestSectionJassim A.Al-Saadi NASATechnicalPaper33341993WallInterference andBoundarySimulationinaTransonicWind TunnelWith a Discretely SlottedTestSectionJassim
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3314.ps.Z, 19980108 NASATechnicalPaper3314June 1993Evaluationof FourAdvancedNozzleConceptsfor Short TakeoffandLandingPerformanceP.FrankQuinto,GuyT. Kemmerly,andJohn W.Paulson, Jr. NASATechnicalPaper33141993Evaluationof FourAdvancedNozzleConceptsfor Short TakeoffandLandingPerformanceP.FrankQuinto,GuyT. Kemmerly,andJohn
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/tm/NASA-98-tm206282.ps.Z, 19980109 NASA/TM-1998-206282Compositional Effects onElectromechanical Degradation ofRAINBOW ActuatorsDavid E. Dausch and Stephanie A. WiseLangley Research Center, Hampton, VirginiaJanuary 1998 The NASA STI Program Office . . . in ProfileSince its founding, NASA has been dedicatedto the advancement of aeronautics
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3367.ps.Z, 19980112 NASATechnicalPaper3367September1993Vibrational RelaxationinHypersonic FlowFieldsWillard E.Meador,GildaA.Miner,andJohn H.Heinbockel NASATechnicalPaper33671993Vibrational RelaxationinHypersonic FlowFieldsWillard E.MeadorandGildaA.MinerLangleyResearchCenterHampton,VirginiaJohn
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr206285.ps.Z, 19980112 December 1997NASA/CR-97-206285Digital PIV (DPIV) Software AnalysisSystemJames L. BlackshireViGYAN, Inc., Hampton, Virginia The NASA STI Program Office ... in ProfileSince its founding, NASA has been dedicatedto the advancement of aeronautics and spacescience. The NASA Scientific and TechnicalInformation
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3358.ps.Z, 19980112 NASATechnicalPaper3358November1993Experimental CavityPressureMeasurementsatSubsonic andTransonicSpeedsStatic-PressureResultsE.B. Plentovich,RobertL. Stallings,Jr.,andM. B.Tracy NASATechnicalPaper33581993Experimental CavityPressureMeasurementsatSubsonic andTransonicSpeedsStatic-PressureResultsE.B.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3365.ps.Z, 19980112 NASATechnicalPaper3365November1993An Experimental InvestigationofaMach3.0High-SpeedCivilTransportatSupersonicSpeedsGloriaHernandez,Peter F.Covell, andMarvin E.McGraw, Jr. NASATechnicalPaper33651993An Experimental
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3350.ps.Z, 19980112 NASATechnicalPaper3350August1993SemiempiricalFragmentationModels onGalacticCosmicRayTransportCalculationsWith Hydrogen TargetJudy L.Shinn,John W.Wilson,andFrancisF.Badavi NASATechnicalPaper33501993SemiempiricalFragmentationModels onGalacticCosmicRayTransportCalculationsWith Hydrogen TargetJudy
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3368.ps.Z, 19980112 NASATechnicalPaper3368September1993RoomTemperatureDegradationofYBa2Cu3O7--xSuperconductorsinVaryingRelativeHumidity EnvironmentsM. W.Hooker,S.A. Wise,I. A.Carlberg,R.M.Stephens,R.T. Simchick,and A.Farjami
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3362.ps.Z, 19980112 NASATechnicalPaper3362CECOMTechnicalReport93-E-2August1993AnalysisofMicrostripPatchAntennas WithNonzeroSurfaceResistanceDavidG.ShivelyandM. C.Bailey NASATechnicalPaper3362CECOMTechnicalReport93-E-21993AnalysisofMicrostripPatchAntennas WithNonzeroSurfaceResistanceDavidG.ShivelyJoint ResearchProgram
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3351.ps.Z, 19980112 NASATechnicalPaper3351August1993CellularTrackModelforStudyofHeavy IonBeamsJudy L.Shinn,RobertKatz,Francis A.Cucinotta,John W.Wilson,andDucM. Ngo NASATechnicalPaper33511993CellularTrackModelforStudyofHeavy IonBeamsJudy
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3349.ps.Z, 19980112 NASATechnicalPaper3349October1993Verification ofFault-TolerantClockSynchronizationSystemsPaulS. Miner NASATechnicalPaper33491993Verification ofFault-TolerantClockSynchronizationSystemsPaulS. MinerLangleyResearchCenterHampton,Virginia NASATechnicalPaper3349
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3361.ps.Z, 19980112 NASATechnicalPaper3361September1993AnalysisofElectromagneticScatteringFromIrregularlyShaped,Thin,MetallicFlatPlatesManohar D.Deshpande,C.R. Cockrell,Fred B.Beck,ErikVedeler,andMelissaB.Koch NASATechnicalPaper33611993AnalysisofElectromagneticScatteringFromIrregularlyShaped,Thin,MetallicFlatPlatesManohar
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3354.ps.Z, 19980112 NASATechnicalPaper3354November1993CalculationsofCosmic-Ray HeliumTransportinShielding MaterialsFrancis A.Cucinotta NASATechnicalPaper33541993CalculationsofCosmic-Ray HeliumTransportinShielding MaterialsFrancis A.CucinottaLangleyResearchCenterHampton,Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr206286.ps.Z, 19980112 December 1997NASA/CR-97-206286PIV/HPIV Film Analysis SoftwarePackageJames L. BlackshireViGYAN, Inc., Hampton, Virginia The NASA STI Program Office ... in ProfileSince its founding, NASA has been dedicatedto the advancement of aeronautics and spacescience. The NASA Scientific and TechnicalInformation
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3355.ps.Z, 19980112 NASATechnicalPaper3355June 1993SupersonicAerodynamicCharacteristicsof anAdvancedF-16DerivativeAircraftConfigurationMike C.FoxandDanaK.Forrest NASATechnicalPaper33551993SupersonicAerodynamicCharacteristicsof anAdvancedF-16DerivativeAircraftConfigurationMike C.FoxViGYAN,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3370.ps.Z, 19980112 NASATechnicalPaper3370December1993Studies ofShuttle OrbiterArrestment SystemPamela A.DavisandSandyM.Stubbs NASATechnicalPaper33701993Studies ofShuttle OrbiterArrestment SystemPamela A.DavisandSandyM.StubbsLangleyResearchCenterHampton,Virginia
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3353.ps.Z, 19980112 NASATechnicalPaper3353August1993Final State Interactions andInclusive Nuclear CollisionsFrancis A.CucinottaandRajendra R.Dubey NASATechnicalPaper33531993Final State Interactions andInclusive Nuclear CollisionsFrancis A.CucinottaLangleyResearchCenterHampton,VirginiaRajendra
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3369.ps.Z, 19980112 NASATechnicalPaper3369September1993Effects of InternalYaw-VectoringDeviceson theStatic PerformanceofaPitch-Vectoring NonaxisymmetricConvergent-Divergent NozzleScott C.Asbury NASATechnicalPaper33691993Effects of InternalYaw-VectoringDeviceson theStatic PerformanceofaPitch-Vectoring
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3352.ps.Z, 19980112 NASATechnicalPaper3352August1993CoulombEffectsinLow-EnergyNuclearFragmentationJohn W.Wilson,Sang Y.Chun,Francis F.Badavi,andSarahJohn NASATechnicalPaper33521993CoulombEffectsinLow-EnergyNuclearFragmentationJohn W.Wilson,LangleyResearchCenterHampton,VirginiaSang
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4413.ps.Z, 19980113 NASATechnicalMemorandum4413Experimental AerodynamicCharacteristicsof aGenericHypersonic AcceleratorConfiguration atMachNumbers 1.5and2.0Ira J.Walker,Peter F.Covell,andDanaK.ForrestFEBRUARY1993 NASATechnicalMemorandum4413Experimental AerodynamicCharacteristicsof aGenericHypersonic
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4435.ps.Z, 19980113 NASATechnicalMemorandum4435Hypersonic LateralandDirectionalStabilityCharacteristics ofAeroassistFlightExperimentConfiguration inAir andCF4John R.Micol andWilliamL.WellsMAY 1993 NASATechnicalMemorandum4435Hypersonic LateralandDirectionalStabilityCharacteristics ofAeroassistFlightExperimentConfiguration
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4421.ps.Z, 19980113 NASATechnicalMemorandum4421PositronLifetimeSpectroscopyfor InvestigationofThin Polymer CoatingsJagJ.Singh,Abe Eftekhari,andDannyR. SprinkleFEBRUARY1993 NASATechnicalMemorandum4421PositronLifetimeSpectroscopyfor InvestigationofThin Polymer
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4406.ps.Z, 19980113 NASATechnicalMemorandum4406AutomaticComputation ofWing-FuselageIntersectionLinesandFillet InsertsWith Fixed-AreaConstraintRaymond L.Barger and MaryS. AdamsFEBRUARY1993 NASATechnicalMemorandum4406AutomaticComputation ofWing-FuselageIntersectionLinesandFillet InsertsWith Fixed-AreaConstraintRaymond
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4438.ps.Z, 19980113 NASATechnicalMemorandum4438Concepts forConformalandBody-AxisAttitudeInformationfor SpatialAwareness PresentedinaHelmet-MountedDisplayDenise R.Jones,TerenceS.Abbott,andJamesR. BurleyIIMARCH1993 NASATechnicalMemorandum4438Concepts forConformalandBody-AxisAttitudeInformationfor SpatialAwareness
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm4790.ps.Z, 19980113 NASA Technical Memorandum 4790PLATSIM: A Simulation and AnalysisPackage for Large-Order Flexible Systems(Version 2.0)Peiman G. Maghami, Sean P. Kenny, and Daniel P. GiesyLangley Research Center, Hampton, VirginiaDecember 1997 The NASA STI Program Office . . . in ProfileSince its founding, NASA has been
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3386.ps.Z, 19980113 NASATechnicalPaper3386CECOMTechnicalReport93-E-1October1993Resonant FrequenciesofIrregularly ShapedMicrostripAntennasUsingMethodofMomentsManohar D.Deshpande,DavidG.Shively,andC.R. Cockrell NASATechnicalPaper3386CECOMTechnicalReport93-E-11993Resonant FrequenciesofIrregularly
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4441.ps.Z, 19980113 NASATechnicalMemorandum4441Assessment ofaFlow-ThroughBalancefor HypersonicWindTunnel ModelsWithScramjetExhaustFlow SimulationLawrence D.Huebner,Marc W.Kniskern,andWilliamJ.MontaAPRIL1993 NASATechnicalMemorandum4441Assessment ofaFlow-ThroughBalancefor HypersonicWindTunnel ModelsWithScramjetExhaustFlow
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4419.ps.Z, 19980113 NASATechnicalMemorandum4419TransitionAerodynamicsfor 20-Percent-Scale VTOLUnmanned Aerial VehicleKevinJ.Kjerstad and JohnW.Paulson,Jr.APRIL1993 NASATechnicalMemorandum4419TransitionAerodynamicsfor 20-Percent-Scale VTOLUnmanned Aerial VehicleKevinJ.Kjerstad and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4407.ps.Z, 19980113 NASATechnicalMemorandum4407Total TemperatureProbes forHigh-TemperatureHypersonicBoundary-LayerMeasurementsCindyW. Albertson and WillardA. Bauserman, Jr.MARCH 1993 NASATechnicalMemorandum4407Total TemperatureProbes forHigh-TemperatureHypersonicBoundary-LayerMeasurementsCindyW. Albertson and WillardA.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4436.ps.Z, 19980113 NASATechnicalMemorandum4436CharacterizationofCavity FlowFields UsingPressure DataObtained inthe Langley 0.3-MeterTransonicCryogenicTunnelM. B.TracyandE.B. PlentovichMARCH1993 NASATechnicalMemorandum4436CharacterizationofCavity FlowFields UsingPressure DataObtained inthe Langley
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/tm/NASA-97-tm206287.ps.Z, 19980113 December 1997NASA/TM-97-206287A Web-Based System for Monitoring andControlling Multidisciplinary DesignProjectsAndrea O. Salas and James L. RogersLangley Research Center, Hampton, Virginia The NASA STI Program Office ... in ProfileSince its founding, NASA has been dedicatedto the advancement of
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3402.ps.Z, 19980113 NASATechnicalPaper3402December1993SurfaceCompositionalVariationsof Mo-47ReAlloyasaFunctionofTemperatureS.J.Hoekje,R.A. Outlaw,andS.N. Sankaran NASATechnicalPaper34021993SurfaceCompositionalVariationsof Mo-47ReAlloyasaFunctionofTemperatureS.J.HoekjeAnalyticalServices&MaterialsHampton,VirginiaR.A.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4412.ps.Z, 19980113 NASATechnicalMemorandum4412Controls-Structures InteractionGuestInvestigatorProgramOverview and Phase I ExperimentalResults and FuturePlansRudeenSmith-TaylorandSharonE.TannerFEBRUARY1993 NASATechnicalMemorandum4412Controls-Structures InteractionGuestInvestigatorProgramOverview and Phase I
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4443.ps.Z, 19980113 NASATechnicalMemorandum4443PolarizationCorrectionforIonizationLossin a GalacticCosmic Ray Transport Code(HZETRN)Judy L.Shinn,HamidullahFarhat,Francis F.Badavi,andJohn W.WilsonMARCH1993 NASATechnicalMemorandum4443PolarizationCorrectionforIonizationLossin a GalacticCosmic Ray Transport Code(HZETRN)Judy
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4442.ps.Z, 19980113 NASATechnicalMemorandum4442Variational TrajectoryOptimizationTool SetTechnical Descriptionand User's ManualRobert R. Bless,EricM. Queen,MichaelD.Cavanaugh,ToddA.WetzelandDanielD.MoerderJULY1993 NASATechnicalMemorandum4442Variational TrajectoryOptimizationTool SetTechnical Descriptionand User's
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4440.ps.Z, 19980113 NASATechnicalMemorandum4440AHigh-Fidelity,Six-Degree-of-FreedomBatchSimulationEnvironmentforTacticalGuidanceResearch and EvaluationKennethH. GoodrichJULY1993 NASATechnicalMemorandum4440AHigh-Fidelity,Six-Degree-of-FreedomBatchSimulationEnvironmentforTacticalGuidanceResearch and EvaluationKennethH.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4422.ps.Z, 19980113 NASATechnicalMemorandum4422Effects of RadiobiologicalUncertaintyonShield Designfor a 60-DayLunarMissionJohn W.Wilson,John E.Nealy,andWalter SchimmerlingJANUARY1993 NASATechnicalMemorandum4422Effects of RadiobiologicalUncertaintyonShield Designfor a 60-DayLunarMissionJohn W.Wilson and JohnE.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4409.ps.Z, 19980113 NASATechnicalMemorandum4409Application of Laser DopplerVelocimetertoChemical VaporLaserSystemLuther R.Gartrell,BagherM. Tabibi,WilliamW. Hunter, Jr., JaH.Lee,andMarkT.FletcherJANUARY1993 NASATechnicalMemorandum4409Application of Laser DopplerVelocimetertoChemical VaporLaserSystemLuther
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4420.ps.Z, 19980113 NASATechnicalMemorandum4420Developmentof aLarge-Scale,Outdoor,Ground-BasedTestCapabilityfor EvaluatingtheEffectofRain onAirfoilLiftGaudyM.BezosandBryanA. CampbellAPRIL1993 NASATechnicalMemorandum4420Developmentof aLarge-Scale,Outdoor,Ground-BasedTestCapabilityfor EvaluatingtheEffectofRain
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4411.ps.Z, 19980113 NASATechnicalMemorandum4411ComputationalParametric Studyof Sidewall-Compression ScramjetInlet Performance atMach10Scott D.HollandFEBRUARY1993 NASATechnicalMemorandum4411ComputationalParametric Studyof Sidewall-Compression ScramjetInlet Performance atMach10Scott
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3404.ps.Z, 19980113 NASATechnicalPaper3404December1993Optical ModelAnalysesofGalacticCosmicRayFragmentationinHydrogenTargetsLawrence W.Townsend NASATechnicalPaper34041993Optical ModelAnalysesofGalacticCosmicRayFragmentationinHydrogenTargetsLawrence W.TownsendLangleyResearchCenterHampton,Virginia SymbolsAnuclearmassnumber
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4408.ps.Z, 19980113 NASATechnicalMemorandum4408TargetFragmentation inRadiobiologyJohn W.Wilson,FrancisA.Cucinotta,Judy L.Shinn,andLawrenceW. TownsendFEBRUARY1993 NASATechnicalMemorandum4408TargetFragmentation inRadiobiologyJohn W.Wilson,FrancisA.Cucinotta,Judy L.Shinn,andLawrenceW.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4434.ps.Z, 19980113 NASATechnicalMemorandum4434Experimental EffectsofWingLocationon Wing-BodyPressuresatSupersonic SpeedsJerry M.AllenandCarolynB. WatsonAPRIL 1993 NASATechnicalMemorandum4434Experimental EffectsofWingLocationon Wing-BodyPressuresatSupersonic SpeedsJerry M.AllenandCarolynB.
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tp3391.ps.Z, 19980113 NASATechnicalPaper3391November1993EffectofTemperatureandO-Ring GlandFinishon SealingAbilityof Viton V747-75CynthiaL.Lach NASATechnicalPaper33911993EffectofTemperatureandO-Ring GlandFinishon SealingAbilityof Viton V747-75CynthiaL.LachLangleyResearchCenterHampton,Virginia Theuseof trademarks ornames of
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4450.ps.Z, 19980113 NASATechnicalMemorandum4450StaticInternalPerformanceofaSingleExpansion RampNozzleWithMultiaxisThrust VectoringCapabilityFrancis J.Capone andAlberto W.SchirmerJULY1993 NASATechnicalMemorandum4450StaticInternalPerformanceofaSingleExpansion RampNozzleWithMultiaxisThrust VectoringCapabilityFrancis
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4519.ps.Z, 19980114 NASATechnicalMemorandum4519ApproximateGreen'sFunctionMethodsforHZETransportinMultilayeredMaterialsJohn W.Wilson,FrancisF.Badavi,Judy L.Shinn,andRobert C.CostenOCTOBER1993 NASATechnicalMemorandum4519ApproximateGreen'sFunctionMethodsforHZETransportinMultilayeredMaterialsJohn
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4520.ps.Z, 19980114 NASATechnicalMemorandum4520Hazard CalculationsofDiffuseReflected Laser Radiationforthe SELENEProgramGildaA.MinerandPhillipD.BabbOCTOBER1993 NASATechnicalMemorandum4520Hazard CalculationsofDiffuseReflected Laser Radiationforthe
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4496.ps.Z, 19980114 NASATechnicalMemorandum4496PowerTransmissionbyLaserBeamFrom Lunar-SynchronousSatelliteM. D.Williams, R.J.De Young,G. L.Schuster,S. H. Choi,J. E.Dagle,E. P.Coomes,Z. I.Antoniak,J.A. Bamberger,J. M.Bates,M. A.Chiu, R.E.Dodge,andJ.A. WiseNOVEMBER1993
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4522.ps.Z, 19980114 NASATechnicalMemorandum4522Energy-LossCrossSectionsfor InclusiveCharge-ExchangeReactions atIntermediate EnergiesFrancis A.Cucinotta,Lawrence W.Townsend,andRajendra R.DubeyOCTOBER1993 NASATechnicalMemorandum4522Energy-LossCrossSectionsfor InclusiveCharge-ExchangeReactions atIntermediate EnergiesFrancis
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4479.ps.Z, 19980114 NASATechnicalMemorandum4479Schlieren PhotographsandInternalPressure Distributionsfor Three-DimensionalSidewall-Compression ScramjetInletsataMachNumberof6inCF4Scott D.HollandAUGUST 1993 NASATechnicalMemorandum4479Schlieren PhotographsandInternalPressure Distributionsfor
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm104092.ps.Z, 19980114 INTRODUCTION TO THELaRC CENTRAL SCIENTIFIC COMPUTING COMPLEXbyJohn N ShoosmithNovember, 1993Central Scientific Computing ComplexDocument A-1f DOCUMENT A-1fTable of ContentsCHAPTER 1. INTRODUCTION.........................................................................................................11.1
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4529.ps.Z, 19980114 NASATechnicalMemorandum4529AerodynamicCharacteristicsandPressure Distributionsfor anExecutive-JetBaselineAirfoil SectionDennis O.Allison and RaymondE. MineckDECEMBER1993 NASATechnicalMemorandum4529AerodynamicCharacteristicsandPressure Distributionsfor anExecutive-JetBaselineAirfoil SectionDennis
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4461.ps.Z, 19980114 NASATechnicalMemorandum4461Optical ModelCalculationsof14.6AGeVSiliconFragmentationCrossSectionsLawrence W.Townsend, Ferdous Khan,and Ram K.TripathiMAY 1993 NASATechnicalMemorandum4461Optical ModelCalculationsof14.6AGeVSiliconFragmentationCrossSectionsLawrence
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/mtg/NASA-97-utsis-ksb.ps.Z, 19980114 NASA Langley Research Center, Hampton, VA K. S. Brentner 1 Helicopter Rotor Noise Prediction: Background, Current Status, and Future Direction Kenneth S. Brentner NASA Langley Research Center Seminar presented at the University of Tennessee Space Institute December 10, 1997 NASA Langley Research Center,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4457.ps.Z, 19980114 NASATechnicalMemorandum4457PhysicalPropertiesof theBenchmark ModelsProgramSupercriticalWingBryanE. Dansberry,MichaelH.Durham,RobertM.Bennett,DavidL. Turnock,Walter A.Silva, andJose A.Rivera,Jr.SEPTEMBER1993 NASATechnicalMemorandum4457PhysicalPropertiesof theBenchmark
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4487.ps.Z, 19980114 NASATechnicalMemorandum4487An ExpertSystemExecutivefor AutomatedAssemblyofLargeSpaceTrussStructuresCherylL. AllenNOVEMBER1993 NASATechnicalMemorandum4487An ExpertSystemExecutivefor AutomatedAssemblyofLargeSpaceTrussStructuresCherylL. AllenLangleyResearchCenterHampton,Virginia Theuseof trademarks ornames
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4488.ps.Z, 19980114 NASATechnicalMemorandum4488Wind TunnelInvestigationofThreeAxisymmetricCowlsofDifferent Lengths atMachNumbers From0.60 to0.92RichardJ.Re and William K.AbeyounisSEPTEMBER1993 NASATechnicalMemorandum4488Wind TunnelInvestigationofThreeAxisymmetricCowlsofDifferent Lengths atMachNumbers From0.60
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4460.ps.Z, 19980114 NASATechnicalMemorandum4460EnhancedReductionofVelocityData ObtainedDuringCETAFlightExperimentTomD. Finley,DouglasT. Wong,and John S.TrippMAY 1993 NASATechnicalMemorandum4460EnhancedReductionofVelocityData ObtainedDuringCETAFlightExperimentTomD. Finley,DouglasT. Wong,and John
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4462.ps.Z, 19980114 NASATechnicalMemorandum4462Comparisonsof Cross-SectionPredictions forRelativisticIronandArgon BeamsWith SemiempiricalFragmentationModelsLawrence W.Townsend, RamK. Tripathi,and FerdousKhanMAY 1993 NASATechnicalMemorandum4462Comparisonsof Cross-SectionPredictions forRelativisticIronandArgon BeamsWith
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4489.ps.Z, 19980114 NASATechnicalMemorandum4489Open Environments ToSupportSystemsEngineeringToolIntegration:AStudyUsingthe PortableCommon ToolEnvironment(PCTE)Dave E.Eckhardt,Jr.,MichaelJ.Jipping,ChrisJ.Wild,StevenJ. Zeil,andCathyC.RobertsSEPTEMBER1993 NASATechnicalMemorandum4489Open Environments
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4497.ps.Z, 19980114 NASATechnicalMemorandum4497Experimental InvestigationofGenericThree-DimensionalSidewall-CompressionScramjetInlets at Mach 6in TetrafluoromethaneScott D.HollandDECEMBER1993 NASATechnicalMemorandum4497Experimental InvestigationofGenericThree-DimensionalSidewall-CompressionScramjetInlets at Mach 6in
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm107684.ps.Z, 19980114 Approaches to High Aspect Ratio TriangulationsMary-Anne K. PosenauNASA Langley Research CenterHampton, Virginiam.a.k.p osenau@larc.nasa.govAbstractIn aerospace computational fluid dynamics calculations, high aspect ratio, or stretched,triangulations are often used to adequately resolve the features of a
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/93/tm4444.ps.Z, 19980114 NASATechnicalMemorandum4444AProposed PerformanceIndexfor Galactic CosmicRayShieldingMaterialsJohn W.Wilson,J.S.Wood, JudyL.Shinn,Francis A.Cucinotta,andJohnE.NealyAUGUST 1993 NASATechnicalMemorandum4444AProposed PerformanceIndexfor Galactic CosmicRayShieldingMaterialsJohn W.Wilson,J.S.Wood,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/tp/NASA-98-tp206290.ps.Z, 19980115 NASA/TP-1998-206290The NASA Monographs on Shell StabilityDesign RecommendationsA Review and Suggested ImprovementsMichael P. Nemeth and James H. Starnes, Jr.Langley Research Center, Hampton, VirginiaJanuary 1998 The NASA STI Program Office . . . in ProfileSince its founding, NASA has been dedicatedto
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/tm/NASA-98-tm206281.ps.Z, 19980116 NASA/TM-1998-206281ARL-TR-1401Wind-Tunnel Evaluation of the Effect ofBlade Nonstructural Mass Distribution onHelicopter Fixed-System LoadsMatthew L. Wilbur, William T. Yeager, Jr., Jeffrey D. Singleton, Paul H. Mirick,and W.Keats WilkieVehicle Technology CenterU.S. Army Research LaboratoryLangley
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/aiaa/NASA-aiaa-98-0170.ps.Z, 19980118 AIAA 98 0170 Aerothermal Heating Predictions for Mars Microprobe R. A. Mitcheltree, M. DiFulvio, T. J. Horvath, and R. D. Braun NASA Langley Research Center, Hampton, Virginia 36th Aerospace Sciences Meeting January 12 15, 1998/Reno, NV For permission to copy or republish, contact the American Institute
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm109152.ps.Z, 19980120 NASA Technical Memorandum 109152Wind-Tunnel Blockage and ActuationSystems Test of a Two-DimensionalScramjet Inlet Unstart Model atMach 6Scott D. HollandLangley Research Center, Hampton, VirginiaNovember 1994National Aeronautics andSpace AdministrationLangley Research CenterHampton, Virginia 23681-0001
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/94/tm4607.ps.Z, 19980120 NASATechnical Memorandum 4607AutomaticProceduresforComputingCompleteConfiguration GeometryFromIndividualComponent DescriptionsRaymondL.BargerandMaryS.AdamsJuly1994 NASATechnical Memorandum 4607AutomaticProceduresforComputingCompleteConfiguration GeometryFromIndividualComponent
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/aiaa/NASA-aiaa-98-0328.ps.Z, 19980121 AIAA 98-0328BOUNDARY LAYER FLOW CONTROL WITH A ONE ATMOSPHERE UNIFORM GLOW DISCHARGE SURFACE PLASMAJ. Reece Roth and Daniel M. ShermanUniversity of Tennessee, Knoxville, TNand Stephen P. WilkinsonNASA Langley Research CenterHampton, VA36th Aerospace Sciences Meeting & ExhibitJanuary 12-15, 1998 / Reno,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/aiaa/NASA-aiaa-98-0880.ps.Z, 19980121 AIAA 98 0880 Aeroheating Predictions for X-34 Using an Inviscid-Boundary Layer Method Christopher J. Riley and William L. Kleb NASA Langley Research Center, Hampton, VA 23681 Steven J. Alter Lockheed Martin Engineering & Sciences, Hampton, VA 23681 36th Aerospace Sciences Meeting & Exhibit January 12
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr206901.ps.Z, 19980122 December 1997NASA/CR-97-206901A User s Guide to the Zwikker-KostenTransmission Line Code (ZKTL)J. J. Kelly and H. Abu-Khajeel The NASA STI Program Office ... in ProfileSince its founding, NASA has been dedicatedto the advancement of aeronautics and spacescience. The NASA Scientific and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/mtg/NASA-98-7seams-lhc.ps.Z, 19980122 ____________________________________________ * Corresponding author address: Lin H. Chambers, Atmospheric Sciences Division, Mail Stop 420, NASA Langley Research Center, Hampton, Virginia 23681- 0001; e-mail . THE CERES S COOL PROJECT: DEVELOPMENT AND OPERATIONAL PHASES Lin
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/aiaa/NASA-aiaa-98-0879.ps.Z, 19980122 AIAA 98 0879 Computational Aeroheating Predictions for X-34 William L. Kleb, William A. Wood, and Peter A. Gnoffo NASA Langley Research Center, Hampton, Virginia 23681 Stephen J. Alter Lockheed Martin Engineering & Sciences, Hampton, Virginia 23681 36th AIAA Aerospace Sciences Meeting and Exhibit
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr206284.ps.Z, 19980123 December 1997NASA/CR-97-206284COMET-AR User s ManualCOmputational MEchanics Testbed With Adaptive RefinementE. Moas, EditorApplied Research Associates, Inc., Raleigh, North Carolina The NASA STI Program Office ... in ProfileSince its founding, NASA has been dedicatedto the advancement of aeronautics and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/tm/NASA-98-tm206283.ps.Z, 19980123 January 1998NASA/TM-1998-206283Flight Demonstration of IntegratedAirport Surface Movement TechnologiesSteven D. Young and Denise R. JonesLangley Research Center, Hampton, Virginia The NASA STI Program Office ... in ProfileSince its founding, NASA has been dedicatedto the advancement of aeronautics and
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tm109171.ps.Z, 19980126 NASA Technical Memorandum 109171A Crew-Centered Flight DeckDesign Philosophy for High-SpeedCivil Transport (HSCT) AircraftMichael T. PalmerLangley Research Center, Hampton, VirginiaWilliam H. RogersBolt, Beranek, & Newman, Inc., Cambridge, MassachusettsHayes N. PressLockheed Engineering & Sciences
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/cr/NASA-97-cr206291.ps.Z, 19980126 December 1997NASA/CR-97-206291Use of Marker Bands for Determination ofFatigue Crack Growth Rates and CrackFront Shapes in Pre-Corroded CouponsS. A. WillardLockheed Martin Engineering and Sciences Services, Hampton, Virginia The NASA STI Program Office ... in ProfileSince its founding, NASA has been
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/mtg/NASA-98-arms-sjb.ps.Z, 19980127 RF 98RM-014: RF1 A novel solution-technique applied to a novel WAASarchitectureSalvatore J. Bavuso NASA HamptonKey Words: Weibull, Reliability, Monte Carlo, simulation, importance sampling, HARP (Hybrid Automated Reliability Prediction), Fault tree, HIRel (HARP integrated Reliability tool system), WAAS,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/95/NASA-95-tp3480.ps.Z, 19980128 NASATechnical Paper 3480Application of Navier-StokesCodePAB3D Withk- "TurbulenceModel to AttachedandSeparated FlowsKhaledS.Abdol-Hamid,B. Lakshmanan,andJohnR.CarlsonJanuary 1995 NASATechnical Paper 3480Application of Navier-StokesCodePAB3D Withk- "TurbulenceModel to AttachedandSeparated
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/tm/NASA-98-tm206913.ps.Z, 19980130 February 1998NASA/TM-1998-206913Evaluation of Heating Methods forThermal Structural Testing of LargeStructuresKamran Daryabeigi, Joseph G. Sikora and Darrell L. Caldwell, Jr.Langley Research Center, Hampton, Virginia The NASA STI Program Office ... in ProfileSince its founding, NASA has been dedicatedto
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/mtg/NASA-98-staif-msl.ps.Z, 19980202 RESEARCH ON THE PROBLEM OF HIGH-PRECISION DEPLOYMENT FOR LARGE-APERTURE SPACE-BASED SCIENCE INSTRUMENTS Mark S. Lake NASA Langley Research Center Hampton, Virginia 23681 757-864-3114 Lee D. Peterson, M. Roman Hachkowski, Jason D. Hinkle, and Lisa R. Hardaway University of Colorado Boulder, Colorado
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/mtg/NASA-98-staif-tfj.ps.Z, 19980205 THERMAL STRUCTURES TECHNOLOGY DEVELOPMENT FOR REUSABLE LAUNCH VEHICLE CRYOGENIC PROPELLANT TANKSTheodore F. JohnsonRoderick NatividadH. Kevin RiversRussell SmithMS 396NASA, Langley Research CenterHampton, VA 23681-0001(757) 864-5418, 864-4204, 864-5428, and 864-3122Abstract Analytical and experimental
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/aiaa/NASA-aiaa-98-0428.ps.Z, 19980206 AIAA Paper No. 98-0428 Application of a Planar Doppler Velocimetry System to a High Reynolds Number Compressible Jet Michael W. Smith NASA Langley Research Center 36th AIAA Aerospace Sciences Meeting and Exhibit January 12-15, 1998 Reno, Nevada
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/aiaa/NASA-aiaa-98-0589.ps.Z, 19980211 AIAA 98-0589The NASA-Langley Wake Vortex Modelling Effortin Support of an Operational Aircraft SpacingSystemFred H. ProctorNASA Langley Research CenterHampton, Virginia36th Aerospace SciencesMeeting & ExhibitJanuary 12-15, 1998 / Reno NevadaFor permission to copy or republish, contact the American
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/aiaa/NASA-aiaa-98-0712.ps.Z, 19980212 AIAA 98 0712 Reduction and Analysis of Phosphor Thermography Data With the IHEAT Software Package N. Ronald Merski NASA Langley Research Center, Hampton, VA 23681 36th AIAA Aerospace Sciences Meeting and Exhibit January 12 15, 1998/Reno, NV For permission to copy or republish, contact the American
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/tp/NASA-98-tp206908.ps.Z, 19980212 NASA/TP-1998-206908Flow and Turbulence Modeling andComputation of Shock Buffet Onset forConventional and Supercritical AirfoilsRobert E. BartelsLangley Research Center, Hampton, VirginiaFebruary 1998 The NASA STI Program Office . . . in ProfileSince its founding, NASA has been dedicatedto the
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/96/NASA-96-aiaaj-rdj.ps.Z, 19980213 AIAA J., vol. 34, no. 11, 1996, pp. 2432-2434 Simulation of Three-Dimensional Symmetric and Asymmetric Instabilities in Attachment-Line Boundary Layers Ronald D. Josliny NASA Langley Research Center Hampton, Virginia 23681-0001 Introduction ON a swept wing, contamination along the leading edge,
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/tp/NASA-98-tp206912.ps.Z, 19980213 NASA/TP-1998-206912Static Thrust and Vectoring Performance ofa Spherical Convergent Flap Nozzle With aNonrectangular Divergent DuctDavid J. WingLangley Research Center, Hampton, VirginiaFebruary 1998 The NASA STI Program Office . . . in ProfileSince its founding, NASA has been dedicatedto the
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1997/jp/NASA-97-tcfd-rdj.ps.Z, 19980218 Large-Eddy Simulation of Transition to Turbulence in Boundary Layers1 Xiaoli Huai, Department of Mechanical Engineering, University of Maryland, College Park, MD 20742, U.S.A. Ronald D. Joslin, Flow Modeling and Control Branch, NASA Langley Research Center, Hampton, VA 23681, U.S.A. and Ugo Piomelli
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/jp/NASA-98-arfm-rdj.ps.Z, 19980218 Annual Review of Fluid Mechanics 1998: vol. 30: 1-29 1 AIRCRAFT LAMINAR FLOW CONTROLy Ronald D. Joslin Fluid Mechanics and Acoustics Division, NASA Langley Research Center, Hampton, VA 23681-0001; email: R.D.Joslin @ larc.nasa.gov KEY WORDS: boundary-layer control; LFC design tools; insect
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/mtg/NASA-98-sfmc-das.ps.Z, 19980218 1AAS 98-146MARS PATHFINDER ATMOSPHERIC ENTRY RECONSTRUCTIONDavid A. Spencer, Robert C. Blanchard#, Sam W. Thurman,Robert D. Braun , Chia-Yen Peng , Pieter H. Kallemeyn The primary objective of the Mars Pathfinder mission was todemonstrate an innovative, low-cost and reliable method forplacing a
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/aiaa/NASA-aiaa-98-0471.ps.Z, 19980218 36st AerospaceSciencesMeeting& ExhibitJanuary12-15, 1998/Reno,NVFor permissionto copy or republish, contact the AmericanInstitute of Aeronautics and Astronautics1801 Alexander BellDrive,Suite500, Reston, Virginia 20191-4344AIAA 98-0471Design andUse of MicrophoneDirectional ArraysforAeroacoustic
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/tm/NASA-98-tm206288.ps.Z, 19980218 February 1998NASA/TM-1998-206288Hydrostar Thermal and StructuralDeformation Analyses of Antenna ArrayConceptRuth M. Amundsen and Drew J. HopeLangley Research Center, Hampton, Virginia The NASA STI Program Office ... in ProfileSince itsfounding, NASA has been dedicatedto the advancement of aeronautics
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/mtg/NASA-98-sfmc-rmv.ps.Z, 19980218 1AAS 98-145NAVIGATION FLIGHT OPERATIONS FOR MARSPATHFINDERRobin M. Vaughan , Pieter H. Kallemeyn, Jr. , David A. Spencer* ,and Robert D. Braun Senior Member of Engineering Staff, Navigation and Flight Mechanics Section, Jet Propulsion Laboratory,California Institute of Technology, Pasadena, California.*
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/aiaa/NASA-aiaa-98-0784.ps.Z, 19980219 1American Institute of Aeronautics and AstronauticsAIAA-98-0784DIRECT HARMONIC LINEAR NAVIER-STOKES METHODSFOR EFFICIENT SIMULATION OF WAVE PACKETS1C.L. StreettNASA Langley Research CenterHampton, VA, USA1 This paper is declared a work of the U.S. Governmentand is not subject to copyright protection in
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/mtg/NASA-98-iwcref-jww.ps.Z, 19980219 High Altitude Radiations Relevant to the High Speed Civil Transport (HSCT) J. W. Wilson1, P. Goldhagan2, D. L. Maiden1, H. Tai1 1NASA Langley Research Center, Hampton, Virginia 2DOE Environmental Measurements Laboratory, New York, New York The Langley Research Center (LaRC) performed atmospheric
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/aiaa/NASA-aiaa-98-0628.ps.Z, 19980219 1American Institute of Aeronautics and AstronauticsAIAA-98-0628NUMERICAL SIMULATION OF FLUCTUATIONSLEADING TO NOISE IN A FLAP-EDGE FLOWFIELD1C.L. StreettNASA Langley Research CenterHampton, VA, USA1This paper is declared a work of the U.S. Governmentand is not subject to copyright protection in the
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/tm/NASA-98-tm206929.ps.Z, 19980220 February 1998NASA/TM-1998-206929Stress Ratio Effects on Crack OpeningLoads and Crack Growth Rates inAluminum Alloy 2024William T. Riddell and Robert S. PiascikLa ngley Research Center, Hampton, Virginia The NASA STI Program Office ... in ProfileSince itsfounding, NASA has been dedicatedto the
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/aiaa/NASA-aiaa-98-0142.ps.Z, 19980225 AIAA-98-0142 1 American Institute of Aeronautics and Astronautics ACCELERATING GROUND-TEST CYCLE TIME; THE SIX-MINUTE MODEL CHANGE AND OTHER VISIONS FOR THE 21ST CENTURY Jerome T. Kegelman* NASA Langley Research Center Hampton, VA 23681
	ftp://techreports.larc.nasa.gov/pub/techreports/larc/1998/tm/NASA-98-tm206930.ps.Z, 19980227 February 1998NASA/TM-1998-206930Flight Demonstration of IntegratedAirport Surface Technologies forIncreased Capacity and SafetyDenise R. Jones, Steven D. Young, Robert W. Wills, Kathryn A. Smith,Floyd S. Shipman, Wayne H. Bryant, and Dave E. Eckhardt, Jr.Langley Research Center, Hampton, Virginia The