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From the NTRS FAQ: Where do I go for a hardcopy of the report?

  1. AERODYNAMIC DERIVATIVES FOR AN OBLIQUE WING AIRCRAFT ESTIMATED FROM FLIGHT DATA BY USING A MAXIMUM LIKELIHOOD TECHNIQUE , Technical Paper
    Authors: R. E. Maine
    Report Number: NASA-TP-1336
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (1,597 KBytes)
    Report Date: October 1978
    No. Pages: 73


  2. FLIGHT-DETERMINED STABILITY AND CONTROL DERIVATIVES FOR THE F-111 TACT RESEARCH AIRCRAFT , Technical Paper
    Authors: A. G. Sim and R. E. Curry
    Report Number: NASA-TP-1350
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (1,513 KBytes)
    Report Date: October 1978
    No. Pages: 78


  3. FLIGHT TESTS OF A RADIO-CONTROLLED AIRPLANE MODE WITH A FREE-WING, FREE-CANARD CONFIGURATION , Technical Memorandum
    Authors: S. W. Gee
    Report Number: NASA-TM-72853
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
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          PDF (641 KBytes)
    Report Date: January 1978
    No. Pages: 13


  4. AN EFFICIENT ALGORITHM FOR CHOOSING THE DEGREE OF A POLYNOMIAL TO APPROXIMATE DISCRETE NONOSCILLATORY DATA , Technical Memorandum
    Authors: D. R. Hedgley
    Report Number: NASA-TM-72854
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
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          PDF (256 KBytes)
    Report Date: April 1978
    No. Pages: 8


  5. COMPARISON OF CALCULATED AND ALTITUDE-FACILITY-MEASURED THRUST AND AIRFLOW OF TWOPROTOTYPE F100 TURBOFAN ENGINES , Technical Paper
    Authors: F. J. Kurtenbach
    Report Number: NASA-TP-1373
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
    Currently this document is not available on-line.
    From the NTRS FAQ: Where do I go for a hardcopy of the report?
    Report Date: December 1978
    No. Pages: 29


  6. MEASUREMENTS AND PREDICTIONS OF FLYOVER AND STATIC NOISE OF A TF30 AFTERBURNING TURBOFAN ENGINE , Technical Paper
    Authors: F. W. Burcham, Jr., P. L. Lasagna and S. C. Oas (Boeing Com. Airplance Co.)
    Report Number: NASA-TP-1372
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
    Currently this document is not available on-line.
    From the NTRS FAQ: Where do I go for a hardcopy of the report?
    Report Date: December 1978
    No. Pages: 94


  7. COMPARISON OF CONCURRENT STRAIN GAGE- AND PRESSURE TRANSDUCER-MEASURED FLIGHT LOADS ON A LIFTINGREENTRY VEHICLE AND CORRELATION WITH WIND TUNNELPREDICTIONS , Technical Paper
    Authors: M. H. Tang, W. J. Sefic and R. G. Sheldon
    Report Number: NASA-TP-1331
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
    Currently this document is not available on-line.
    From the NTRS FAQ: Where do I go for a hardcopy of the report?
    Report Date: October 1978
    No. Pages: 42


  8. UTILIZATION OF THE WING-BODY AERODYNAMIC ANALYSIS PROGRAM , Technical Memorandum
    Authors: R. E. Curry
    Report Number: NASA-TM-72856
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (870 KBytes)
    Report Date: October 1978
    No. Pages: 29


  9. CORRELATION OF PREDICTED AND MEASURED THERMAL STRESSES ON A TRUSS-TYPE AIRCRAFT STRUCTURE , Technical Memorandum
    Authors: J. M. Jenkins, L. S. Schuster and A. L. Carter
    Report Number: NASA-TM-72857
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
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          PDF (1,551 KBytes)
    Report Date: November 1978
    No. Pages: 57


  10. EFFECT OF SAMPLING RATE AND RECORD LENGTH ON THE DETERMINATION OF STABILITY AND CONTROL DERIVATIVES , Technical Memorandum
    Authors: M. J. Brenner, K. W. Iliff and R. K. Whitman
    Report Number: NASA-TM-72858
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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          PDF (2,292 KBytes)
    Report Date: December 1978
    No. Pages: 140


  11. DIGITAL FLY-BY-WIRE FLIGHT CONTROL VALIDATION EXPERIENCE , Technical Memorandum
    Authors: K. J. Szalai, C. R. Jarvis, G. E. Krier, V. A. Megna, L. D. Brock and R. N. O'Donnell
    Report Number: NASA-TM-72860
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (9,513 KBytes)
    Report Date: December 1978
    No. Pages: 241


  12. FLIGHT EVALUATION OF THE TRANSONIC STABILITY AND CONTROL CHARACTERISTICS OF AN AIRPLANE INCORPORATING A SUPERCRITICAL WING , Technical Paper
    Authors: N. W. Matheny and D. H. Gatlin
    Report Number: NASA-TP-1167
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (1,730 KBytes)
    Report Date: February 1978
    No. Pages: 61


  13. ANALYTICAL STUDY OF RIDE SMOOTHING BENEFITS OF CONTROL SYSTEM CONFIGURATIONS OPTIMIZED FOR PILOT HANDLING QUALITIES , Technical Paper
    Authors: B. G. Powers
    Report Number: NASA-TP-1148
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (1,538 KBytes)
    Report Date: February 1978
    No. Pages: 60


  14. RESULTS FROM FLIGHT AND SIMULATOR STUDIES OF A MACH 3 CRUISE LONGITUDINAL AUTOPILOT , Technical Paper
    Authors: G. B. Gilyard and J. W. Smith
    Report Number: NASA-TP-1180
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (2,642 KBytes)
    Report Date: April 1978
    No. Pages: 85


  15. FLIGHT-MEASURED PRESSURE CHARACTERISTICS OF AFT-FACING STEPS IN HIGH REYNOLDS NUMBER FLOW ATMACH NUMBERS OF 2.20, 2.50, AND 2.80 ANDCOMPARISON WITH OTHER DATA , Technical Memorandum
    Authors: S. G. Powers
    Report Number: NASA-TM-72855
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (1,466 KBytes)
    Report Date: May 1978
    No. Pages: 38


  16. DEVELOPMENT OF SYSTEMS AND TECHNIQUES FOR LANDING AN AIRCRAFT USING ONBOARD TELEVISION , Technical Paper
    Authors: S. W. Gee, P. C. Carr, W. R. Winter and J. A. Manke
    Report Number: NASA-TP-1171
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (1,978 KBytes)
    Report Date: February 1978
    No. Pages: 24


  17. DESIGN AND PHYSICAL CHARACTERISTICS OF THE TRANSONIC AIRCRAFT TECHNOLOGY (TACT) RESEARCHAIRCRAFT , Technical Memorandum
    Authors: W. D. Painter and L. J. Caw
    Report Number: NASA-TM-56048
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (1,506 KBytes)
    Report Date: January 1978
    No. Pages: 32


  18. DRAG REDUCTION OBTAINED BY MODIFYING A STANDARD TRUCK , Technical Memorandum
    Authors: A. E. Sheridan and S. J. Grier
    Report Number: NASA-TM-72846
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (2,607 KBytes)
    Report Date: February 1978
    No. Pages: 28


  19. A STATISTICAL PACKAGE FOR COMPUTING TIME AND FREQUENCY DOMAIN ANALYSIS , Technical Memorandum
    Authors: J. Brownlow
    Report Number: NASA-TM-56045
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (3,072 KBytes)
    Report Date: August 1978
    No. Pages: 80


  20. FLIGHT COMPARISON OF THE TRANSONIC AGILITY OF THE F-111A AIRPLANE AND THE F-111 SUPERCRITICAL WING AIRPLANE , Technical Paper
    Authors: E. L. Friend and G. M. Sakamoto
    Report Number: NASA-TP-1368
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (2,449 KBytes)
    Report Date: December 1978
    No. Pages: 79


  21. FLIGHT-MEASURED BUFFET CHARACTERISTICS OF A SUPERCRITICAL WING AND A CONVENTIONAL WING ON A VARIABLE-SWEEP AIRPLANE , Technical Paper
    Authors: R. C. Monaghan
    Report Number: NASA-TP-1244
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (1,614 KBytes)
    Report Date: May 1978
    No. Pages: 40