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

  1. FLIGHT-DETERMINED AERODYNAMIC STABILITY AND CONTROL DERIVATIVES OF THE M2-F2 LIFTING BODY VEHICLE AT SUBSONIC SPEEDS , Technical Memorandum
    Authors: R. W. Kempel and R. C. Thompson
    Report Number: NASA-TM-X-2413
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (1,519 KBytes)
    Report Date: December 1971
    No. Pages: 35


  2. VERIFICATION OF TAKEOFF PERFORMANCE PREDICTIONS FOR THE XB-70 AIRPLANE , Technical Memorandum
    Authors: T. J. Larson and W. G. Schweikhard
    Report Number: NASA-TM-X-2215
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (1,384 KBytes)
    Report Date: March 1971
    No. Pages: 30


  3. VALIDATION OF A GENERAL PURPOSE AIRBORNE SIMULATOR FOR SIMULATION OF LARGE TRANSPORT AIRCRAFT HANDLING QUALITIES , Technical Note
    Authors: K. J. Szalai
    Report Number: NASA-TN-D-6431
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (3,421 KBytes)
    Report Date: October 1971
    No. Pages: 74


  4. ENGINE EXHAUST NOISE DURING GROUND OPERATION OF THE XB-70 AIRPLANE , Technical Note
    Authors: P. L. Lasagna and T. W. Putnam
    Report Number: NASA-TN-D-7043
    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: January 1971
    No. Pages: 36


  5. COMPARISON OF WIND TUNNEL AND FLIGHT-MEASURED BASE PRESSURES FROM THE SHARP-LEADING-EDGE UPPER VERTICAL FIN OF THE X-15 AIRPLANE FOR TURBULENT FLOW AT MACH NUMBERS FROM 1.5 TO 5.0 , Technical Note
    Authors: S. A. Goecke
    Report Number: NASA-TN-D-6348
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (1,562 KBytes)
    Report Date: May 1971
    No. Pages: 40


  6. FLIGHT EVALUATION OF ANGLE OF ATTACK AS A CONTROL PARAMETER IN GENERAL-AVIATION AIRCRAFT , Technical Note
    Authors: S. W. Gee, H. G. Gaidsick and E. K. Envoldson
    Report Number: NASA-TN-D-6210
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (1,119 KBytes)
    Report Date: March 1971
    No. Pages: 24


  7. EXPERIENCE WITH THE X-15 ADAPTIVE FLIGHT CONTROL SYSTEM , Technical Note
    Authors: Anonymous
    Report Number: NASA-TN-D-6208
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (1,627 KBytes)
    Report Date: March 1971
    No. Pages: 29


  8. INSTRUMENTATION AND DROP-TESTING TECHNIQUES FOR INVESTIGATING FLIGHT VEHICLES AND PERSONNEL PROTECTIVE SYSTEMS , Technical Memorandum
    Authors: R. Carpenter, M. O. Thompson and J. H. Bowers
    Report Number: NASA-TM-X-2149
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (1,157 KBytes)
    Report Date: January 1971
    No. Pages: 20


  9. EVALUATION OF EFFECTS OF HIGH-ALTITUDE TURBULENCE ENCOUNTERS ON THE XB-70 AIRPLANE , Technical Note
    Authors: R. R. Larson, B. J. Love and R J. Wilson
    Report Number: NASA-TN-D-6457
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (3,069 KBytes)
    Report Date: July 1971
    No. Pages: 86


  10. ANALYSIS OF A COUPLED ROLL SPIRAL MODE, PILOT INDUCED OSCILLATION EXPERIENCED WITH THE M2-F2 LIFTING BODY , Technical Note
    Authors: R. W. Kempel
    Report Number: NASA-TN-D-6496
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (2,801 KBytes)
    Report Date: September 1971
    No. Pages: 59


  11. FLIGHT DETERMINED ACCELERATION AND CLIMB PERFORMANCE OF AN F-104G AIRPLANE FORUSE IN AN OPTIMUM FLIGHT PATH COMPUTER PROGRAM , Technical Note
    Authors: R. T. Marshall
    Report Number: NASA-TN-D-6398
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (1,271 KBytes)
    Report Date: June 1971
    No. Pages: 38


  12. IN-FLIGHT USE OF TRAVERSING BOUNDARY-LAYER PROBES , Technical Note
    Authors: E. J. Saltzman
    Report Number: NASA-TN-D-6428
    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: July 1971
    No. Pages: 32


  13. IN-FLIGHT EVALUATION OF THE LATERAL HANDLING OF A FOUR-ENGINE JET TRANSPORT DURING APPROACH AND LANDING , Technical Note
    Authors: G. B. Gilyard and E. C. Holleman
    Report Number: NASA-TN-D-6339
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (1,303 KBytes)
    Report Date: May 1971
    No. Pages: 33


  14. AN INVESTIGATION OF TWO VARIATIONS OF THE GAS GENERATOR METHOD TO CALCULATE THE THRUSTOF THE AFTERBURNING TURBOFAN ENGINES INSTALLED IN AN F-111A AIRPLANE , Technical Note
    Authors: F. W. Burcham, Jr.
    Report Number: NASA-TN-D-6297
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (1,477 KBytes)
    Report Date: April 1971
    No. Pages: 31


  15. MOTION CUE AND SIMULATION FIDELITY ASPECTS OF THE VALIDATION OF A GENERAL PURPOSE AIRBORNE SIMULATOR , Technical Note
    Authors: K. J. Szalai
    Report Number: NASA-TN-D-6432
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (1,672 KBytes)
    Report Date: October 1971
    No. Pages: 37


  16. VERTICAL-FIN LOADS AND RUDDER HINGE-MOMENT MEASUREMENTS ON A 1/8 SCALE MODEL OF THE M2-F3 LIFTING BODY VEHICLE ATMACH NUMBERS FROM 0.50 TO 1.30 , Technical Memorandum
    Authors: M. H. Tang
    Report Number: NASA-TM-X-2286
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (978 KBytes)
    Report Date: May 1971
    No. Pages: 44


  17. DIGITAL AUTOMATIC DATA REDUCTION TECHNIQUES USED IN A 1000-FLIGHT BIOMEDICAL STUDY , Technical Note
    Authors: R. Carpenter and J. Roman
    Report Number: NASA-TN-D-6601
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (768 KBytes)
    Report Date: December 1971
    No. Pages: 17


  18. COMPARISONS OF IN-FLIGHT F-111A INLET PERFORMANCE FOR ON AND OFF SCHEDULED INLETGEOMETRY AT MACH NUMBERS OF 0.68 TO 2.18 , Technical Note
    Authors: D. L. Hughes and R. A. Martin
    Report Number: NASA-TN-D-6490
    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: September 1971
    No. Pages: 47


  19. A STATISTICAL TECHNIQUE FOR COMPUTER IDENTIFICATION OF OUTLIERS IN MULTIVARIATE DATA , Technical Note
    Authors: R. Swaroop and W. R. Winter
    Report Number: NASA-TN-D-6472
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (974 KBytes)
    Report Date: August 1971
    No. Pages: 31


  20. BOUNDARY LAYER TRANSITION DETECTION ON THE X-15 VERTICAL FIN USING SURFACE-PRESSURE-FLUCTUATION MEASUREMENTS , Technical Memorandum
    Authors: T. L. Lewis and R. D. Banner
    Report Number: NASA-TM-X-2466
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (860 KBytes)
    Report Date: December 1971
    No. Pages: 18


  21. FLIGHT-MEASURED HL-10 LIFTING BODY CENTER FIN LOADS AND CONTROL SURFACE HINGE MOMENTS AND CORRELATION WITH WIND-TUNNEL PREDICTIONS , Technical Memorandum
    Authors: M. H. Tang and G. P. E. Pearson
    Report Number: NASA-TM-X-2419
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (1,536 KBytes)
    Report Date: October 1971
    No. Pages: 40