WWC snapshot of http://www.dfrf.nasa.gov/ReportServer/1990/1990-abs-bib.html taken on Sun Jun 4 1:48:26 1995

Bibliography - Dryden Technical Report Server

  1. Gurbux S. Alag and Glenn B. Gilyard, ``A Proposed Kalman Filter Algorithm for Estimation of Unmeasured Output Variables for an F100 Turbofan Engine,'' NASA TM-4234, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, Also presented as AIAA 90-1920 at AIAA/SAE/ASME/ASEE Joint Propulsion Conference, Orlando, FL, July 16-18, 1990, H-1639.

  2. James G. Allen and Scott E. Sikora, ``A Knowledge-Based System Design/Information Tool,'' NASA CR-4316, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, NASA Technical monitor: Dale A. Mackall, H-1621.

  3. Bianca T. Anderson and Robert R. Meyer, Jr., ``Effects of Wing Sweep on Boundary-Layer Transition for a Smooth F-14A Wing at Mach Numbers From 0.700 to 0.825,'' NASA TM-101712, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, Subject category: 34. Microfiche supplement., H-1531.

    Keywords:Boundary-layer transition, Laminar flow, Natural laminar flow

  4. Bianca T. Anderson and Robert R. Meyer, Jr., ``Effects of Wing Sweep on In-Flight Boundary-Layer Transition for a Laminar Flow Wing at Mach Numbers From 0.60 to 0.79,'' NASA TM-101701, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, H-1565.

  5. R. E. Bailey and L. H. Knotts, ``Interaction of Feel System and Flight Control System Dynamics on Lateral Flying Qualities,'' NASA CR-179445, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, NASA Technical monitor: Mary F. Shafer, H-1584.

  6. Jeffrey E. Bauer and Dominick Andrisani, ``Estimating Short-Period Dynamics Using an Extended Kalman Filter,'' NASA TM-101722, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, Also presented as AIAA 90-1277, Ontario, CA, May 1990, H-1625.

  7. Frank W. Burcham, Jr. , Glenn B. Gilyard and Paul A. Gelhausen, ``Integrated Flight-Propulsion Control Concepts for Supersonic Transport Airplanes,'' NASA TM-101728, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, Also presented as paper 901928 at SAE Aerotech '90 Conference, Long Beach, CA, Oct. 1-4, 1990. (Burcham and Gilyard: NASA Dryden; Gelhausen: NASA Ames, Moffett Field, CA) Subject category: 08, H-1673.

    Keywords:F-15, High Speed Civil Transport, Integrated control, Performance seeking control

    Abstract: Integration of propulsion and flight-control systems will provide significant performance improvements for supersonic transport airplanes. Increased engine thrust and reduced fuel consumption can be obtained by controlling engine stall margin as a function of flight and engine operating conditions. Improved inlet pressure recovery and decreased inlet drag can result from inlet control system integration. Using propulsion system forces and moments to augment the flight-control system and airplane stability can reduce the flight-control surface and tail size, weight, and drag. Special control modes may also be desirable for minimizing community noise and for emergency procedures. The overall impact of integrated controls on the takeoff gross weight for a generic high speed civil transport is presented.

  8. Frank W. Burcham, Jr., Glenn B. Gilyard and Lawrence P. Myers, ``Propulsion System/Flight Control Integration and Optimization: Flight Evaluation and Technology Transition,'' NASA TM-4207, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, Also presented as AIAA 90-2280, 26th Joint Propulsion Conference, Orlando, FL, July 16-18,1990. Subject category: 07, H-1603.

    Keywords:F-15, Flight research, Integration, Propulsion, Technology transition, YF-12

  9. Vince Chacon, Joseph W. Pahle and Victoria A. Regenie, ``Validation of the F-18 High Alpha Research Vehicle Flight Control and Avionics Systems Modifications,'' NASA TM-101723, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, Also presented as paper for IEEE 9th Digital Avionics Systems Conference, Virginia Beach, VA, Oct. 15-18, 1990. Subject category: 05, H-1632.

    Keywords:Avionics, Flight control, HARV, Validation

  10. Steven B. Davis, ``Real-Time Application of Advanced Three-Dimensional Graphic Techniques for Research Aircraft Simulation,'' NASA TM-101730, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, H-1642.

  11. V. Michael DeAngelis and Roger A. Fields, ``Techniques for Hot Structures Testing,'' NASA TM-101727, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, Also presented as paper for 1st Thermal Structures Conference, University of Virginia, Charlottesville, VA, Nov. 13-15, 1990, H-1664.

  12. David F. Fisher, D. W. Banks and David M. Richwine, ``F-18 High Alpha Research Vehicle Surface Pressures: Initial In-Flight Results and Correlation With Flow Visualization and and Wind-Tunnel Data,'' NASA TM-101724, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, H-1633.

  13. David F. Fisher, John H. Del Frate and David M. Richwine, ``In-Flight Flow Visualization Characteristics of the NASA F-18 High Alpha Research Vehicle at High Angles of Attack,'' NASA TM-4193, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, H-1576.

  14. John H. Del Frate, David F. Fisher and Fanny A. Zuniga, ``In-Flight Flow Visualization With Pressure Measurements at Low Speeds on the NASA F-18 High Alpha Research Vehicle,'' NASA TM-101726, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, Also presented as paper for AGARD Vortex Flow Aerodynamics Conference, Scheveningen, Netherlands, Oct. 1-4, 1990. Subject category: 02, H-1651.

    Keywords:F-18, Flight test, Flow visualization, High angle of attack, Low speed, Vortex flow

  15. Lawrence C. Freudinger and Michael W. Kehoe, ``Flutter Clearance of the F-14A Variable-Sweep Transition Flight Experiment Airplane ╤ Phase 2,'' NASA TM-101717, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, H-1598.

  16. Edwad L. Friend, ``Initial Flight Buffet Characteristics of the X-29 Airplane Including Comparisons With Other Contemporary Designs ,'' NASA TM-4159, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, H-1503.

  17. K. K. Gupta, ``STARS ╤ An Integrated General-Purpose Finite Element Structural, Aeroelastic, and Aeroservoelastic Analysis Computer Program ,'' NASA TM-101709, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, H-1582.

  18. Edward A. Haering, ``Airdata Calibration of a High-Performance Aircraft for Measuring Atmospheric Wind Profiles,'' NASA TM-101714, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, Also presented as AIAA 90-0230, Reno, NV, Jan. 1990, H-1580.

  19. Steven A. Johnson, ``A Simple Dynamic Engine Model for Use in a Real-Time Aircraft Simulation With Thrust Vectoring ,'' NASA TM-4240, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, Also presented as AIAA 90-2166 at AIAA/SAE/ASME/ASEE Joint Propulsion Conference, Orlando, FL, July 16-18, 1990, H-1643.

  20. Steven A. Johnson and David F. Fisher, ``Water-Tunnel Study Results of a TF/A-18 and F/A-18 Canopy Flow Visualization,'' NASA TM-101705, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, Subject category: 02, H-1570.

    Keywords:Canopy flow, Leading-edge extension, Vortex breakdown, Water tunnel

  21. Michael W. Kehoe, Edward J. Laurie and Lisa J. Bjarke, ``An In-Flight Interaction of the X-29A Canard and Flight Control System,'' NASA TM-101718, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, Also presented as AIAA 90-1240 for Dynamics Specialist Meeting, Long Beach, CA, Apr. 5-6, 1990. (Kehoe and Bjarke: NASA Dryden; Laurie: Grumman Aerospace Corporation, NY). Subject category: 05, H-1590.

    Keywords:Aerodynamics, Aeroservoelasticity, Flight controls, Flight control structure interaction, Forward-swept wing, Structural dynamics

  22. Lura E. Kern, Steven D. Belle and Eugene L. Duke, ``Effects of Simplifying Assumptions on Optimal Trajectory Estimation for a High- Performance Aircraft,'' NASA TM-101721, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, (Kern and Duke: NASA Dryden: Belle: PRC Inc., Edwards, CA) Subject category: 08, H-1597.

    Keywords:Energy state approximation, Simplifying assumptions, Trajectory optimization

  23. William L. Ko and Raymond H. Jackson, ``Open-Mode Delamination Stress Concentrations in Horseshoe and Elliptic Composite Curved Bars Subjected to End Forces,'' NASA TM-4164, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, Subject category: 24, H-1567.

    Keywords:Delamination stresses, Elliptic curved bar, Horseshoe curved bar, Laminated composites, Sandwich laminations, Solid laminations

  24. William L. Ko, Timothy Olona and K. M. Muramoto, ``Optimum Element Density Studies for Finite-Element Thermal Analysis of Hypersonic Aircraft Structures,'' NASA TM-4163, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, H-1519.

  25. Terry J. Larson, Timothy R. Moes and Paul M. Siemers III, ``Wind-Tunnel Investigation of a Flush Airdata System at Mach Numbers From 0.7 to 1.4,'' NASA TM-101697, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, H-1544.

  26. William A. Lokos, ``Predicted and Measured In-Flight Wing Deformations of a Forward-Swept-Wing Aircraft ,'' NASA TM-4245, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, Also presented as paper at SFTE 21st Annual Flight Test Symposium, Garden Grove, CA, Aug. 6-10, 1990, H-1650.

  27. Dale A. Mackall, David McBride and Dorothea Cohen, ``Overview of the NASA Ames-Dryden Integrated Test Facility,'' NASA TM-101720, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, Also presented as paper for 36th Instrument Society of America ASD/TMD Proceedings, Denver, CO, May 7-10, 1990. Subject category: 09, H-1596.

    Keywords:Flight test, Integrated Test Facility, Real-time monitoring, Simulation, Software verification and validation

  28. Timothy R. Moes and Stephen A. Whitmore, ``A Preliminary Look at Techniques Used to Obtain Airdata From Flight at High Angles of Attack,'' NASA TM-101729, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, Also presented as paper for High Angle of Attack Technology Symposium, Hampton, VA, Oct. 30 - Nov. 1, 1990, H-1674.

  29. Timothy R. Moes and Robert R. Meyer, Jr., ``In-Flight Investigation of Shuttle Tile Pressure Orifice Installations,'' NASA TM-4219, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, H-1575.

  30. E. Nissim, ``Design of Control Laws for Flutter Suppression Based on the Aerodynamic Energy Concept and Comparisons With Other Design Methods ,'' NASA TP-3056, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, H-1549.

  31. E. Nissim, ``The Effectiveness of Vane-Aileron Excitation in the Experimental Determination of Flutter Speed by Parameter Identification ,'' NASA TP-2971, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, H-1516.

  32. Nora O'Neill-Rood and Richard D. Glover, ``An Automated Calibration Laboratory for Flight Research Instrumentation: Requirements and a Proposed Design Approach,'' NASA TM-101719, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, Also presented as a paper for 36th ISA International Instrumentation Symposium, Denver, CO, May 7-10, 1990, H-1594.

  33. Joseph W. Pahle, ``Output Model-Following Control Synthesis for an Oblique-Wing Aircraft,'' NASA TM-100454, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, Subject category: 08, H-1522.

    Keywords:Automatic control, Control law synthesis, Model following, Oblique wing

  34. Robert D. Quinn and Les Gong, ``Real-Time Aerodynamic Heating and Surface Temperature Calculations for Hypersonic Flight Simulation,'' NASA TM-4222, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, H-1602.

  35. Ronald J. Ray, ``Evaluation of Various Thrust Calculation Techniques on an F404 Engine,'' NASA TP-3001, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, H-1505.

  36. Scott E. Sikora, ``Model Authoring System for Fail Safe Analysis,'' NASA CR-4317, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, NASA Technical monitor: Dale A. Mackall, H-1620.

  37. Alex G. Sim, ``Flight Characteristics of a Modified Schweizer SGS 1-36 Sailplane at Low and Very High Angles of Attack ,'' NASA TP-3022, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, H-1563.

  38. Joel R. Sitz and Todd H. Vernon, ``Flight Control System Design Factors for Applying Automated Testing Techniques,'' NASA TM-4242, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, Also presented as paper for IEEE 9th Annual Digital Avionics System Conference, Virginia Beach, VA, Oct. 15-18, 1990, H-1631.

  39. James F. Stewart and Thomas L. Shuck, ``Flight-Testing of the Self-Repairing Flight Control System Using the F-15 Highly Integrated Digital Electronic Control Flight Research Facility,'' NASA TM-101725, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, Also presented as AIAA 90-1321 for AIAA/SFTE/DGLR/SETP 5th Biannual Flight Test Conference, Ontario, CA, May 21-24, 1990, H-1635.

  40. David F. Voracek, ``Monitoring Techniques for the X-29A Aircraft's High-Speed Rotating Power Takeoff Shaft ,'' NASA TM-101731, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, Also presented as paper at 2nd International Machinery Monitoring and Diagnostic Conference, Los Angeles, CA, Oct. 22-25, 1990, H-1680.

  41. Stephen A. Whitmore and Cornelius T. Leondes, ``Compensating for Pneumatic Distortion in Pressure Sensing Devices,'' NASA TM-101716, NASA Dryden Flight Research Center, Edwards, CA 93523-0273, 1990, Also presented as AIAA 90-0631, Reno, NV, Jan. 1990, H-1586.

  42. Stephen A. Whitmore, W. T. Lindsey, Robert E. Curry and Glenn B. Gilyard, ``Experimental Characterization of the Effects of Pneumatic Tubing on Unsteady Pressure Measurements,'' NASA TM-4171, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, (Whitmore, Curry, and Gilyard: NASA Dryden; Lindsey: Air Force Wright Aeronautical Laboratory, Wright-Patterson AFB, OH) Subject category: 06, H-1538.

    Keywords:Airdata, Pneumatic lag, Pneumatic tubing, Pressure sensors

  43. Stephen A. Whitmore, Timothy R. Moes and Terry J. Larson, ``Preliminary Results From a Subsonic High Angle-of-Attack Flush Airdata Sensing (HI-FADS) System: Design, Calibration, and Flight Test Evaluation,'' NASA TM-101713, NASA Dryden Flight Research Facility, Edwards, CA 93523-0273, 1990, Also presented as AIAA 90-0232, Reno, NV, Jan. 1990, H-1583.