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From the NTRS FAQ: Where do I go for a hardcopy of the report?
  1. DRAG REDUCTION OBTAINED BY THE ADDITION OF A BOATTAIL TO A BOX SHAPED VEHICLE
    Authors: Randall L. Peterson
    Report Number: NASA-CR-163113
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (1,656 KBytes)
    Report Date: August 1981
    No. Pages: 32


  2. A REVIEW OF FLIGHT-TO-WIND TUNNEL DRAG CORRELATION , Conference Paper
    Authors: Edwin J. Saltzman and Theodore G. Ayers
    Report Number: AIAA812475
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (1,829 KBytes)
    Report Date: November 1981
    No. Pages: 18


  3. PROGRAMMER'S MANUAL FOR MMLE3, A GENERAL FORTRAN PROGRAM FOR MAXIMUM LIKELIHOOD PARAMETER ESTIMATION , Technical Paper
    Authors: R. E. Maine
    Report Number: NASA-TP-1690
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (5,726 KBytes)
    Report Date: June 1981
    No. Pages: 118


  4. FLIGHT EVALUATION OF A SIMPLIFIED GROSS THRUST CALCULATION TECHNIQUE USING AN F100 TURBOFAN ENGINE IN AN F-15 AIRPLANE , Technical Paper
    Authors: F. J. Kurtenbach and F. W. Burcham, Jr.
    Report Number: NASA-TP-1782
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (909 KBytes)
    Report Date: January 1981
    No. Pages: 21


  5. THE THEORY AND PRACTICE OF ESTIMATING THE ACCURACY OF DYNAMIC FLIGHT-DETERMINED COEFFICIENTS , Reference Publication
    Authors: R. E. Maine and K. W. Iliff
    Report Number: NASA-RP-1077
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (2,994 KBytes)
    Report Date: July 1981
    No. Pages: 63


  6. APPLICATION OF A PERFORMANCE MODELING TECHNIQUE TO AN AIRPLANE WITH VARIABLE SWEEP WINGS , Technical Paper
    Authors: P. C. Redin
    Report Number: NASA-TP-1855
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (988 KBytes)
    Report Date: May 1981
    No. Pages: 33


  7. CLIMATOLOGICAL CHARACTERISTICS OF HIGH ALTITUDE WIND SHEAR AND LAPSE RATE LAYERS , Technical Memorandum
    Authors: L. J. Ehernberger and N.B. Guttman
    Report Number: NASA-TM-81353
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (2,560 KBytes)
    Report Date: February 1981
    No. Pages: 99


  8. DIVERSITY TECHNIQUES FOR OMNIDIRECTIONAL TELEMETRY COVERAGE OF THE HIMAT RESEARCH VEHICLE , Technical Paper
    Authors: P. F. Harney
    Report Number: NASA-TP-1830
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (798 KBytes)
    Report Date: March 1981
    No. Pages: 18


  9. COMPARISON OF THREE THRUST CALCULATION METHODS USING IN-FLIGHT THRUST DATA , Technical Memorandum
    Authors: D. L. Hughes
    Report Number: NASA-TM-81360
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (1,090 KBytes)
    Report Date: July 1981
    No. Pages: 35


  10. DESCRIPTION OF THE HIMAT TAILORED COMPOSITE STRUCTURE AND LABORATORY MEASURED VEHICLE SHAPE UNDER LOAD , Technical Memorandum
    Authors: R. C. Monaghan
    Report Number: NASA-TM-81354
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (2,278 KBytes)
    Report Date: February 1981
    No. Pages: 60


  11. HISTORICAL BACKGROUND AND DESIGN EVOLUTION OF THE TRANSONIC AIRCRAFT TECHNOLOGY SUPERCRITICAL WING , Technical Memorandum
    Authors: T. G. Ayers and J. B. Hallissy
    Report Number: NASA-TM-81356
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (1,073 KBytes)
    Report Date: August 1981
    No. Pages: 33


  12. THE DEVELOPMENT AND FLIGHT TEST EVALUATION OF AN INTEGRATED PROPULSION CONTROL SYSTEM FOR THE HIMAT RESEARCH AIRPLANE , Conference Paper
    Authors: J. L. Baer-Riedhart
    Report Number: H-1157
    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: November 1981
    No. Pages: 10


  13. USER'S MANUAL FOR FSLIP-3, FLEXSTAB LOADS INTEGRATION PROGRAM , Technical Memorandum
    Authors: R. L. Sims
    Report Number: NASA-TM-81364
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (3,535 KBytes)
    Report Date: August 1981
    No. Pages: 121


  14. ANALYTIC STUDY OF ORBITER LANDING PROFILES , Technical Memorandum
    Authors: H. J. Walker
    Report Number: NASA-TM-81365
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (3,135 KBytes)
    Report Date: September 1981
    No. Pages: 115


  15. ANALYSIS OF A LONGITUDINAL PILOT-INDUCED OSCILLATION EXPERIENCED ON THE APPROACH AND LANDING TEST OF THE SPACE SHUTTLE , Technical Memorandum
    Authors: J. W. Smith
    Report Number: NASA-TM-81366
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          PDF (1,120 KBytes)
    Report Date: December 1981
    No. Pages: 45
 
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