Research Catalog

  • Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane [microform] / Dennis O. Allision and William G. Sewall.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service (NTIS) [distributor, 1995]
    • 1995
  • Investigation into the impact of agility in conceptual fighter design [microform] / R.M. Engelbeck.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • PARC3D calculations of the F/A-18A HARV inlet vortex generators [microform] / Steve D. Podleski.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Pilot evaluation comments during selected maneuvers from flight tests of the HARV NASA-1A control law [microform] / Jessie C. Yeager.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997
  • Structural dynamic model obtained from flight use with piloted simulation and handling qualities analysis [microform] / Bruce G. Powers.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1996.
    • 1996
  • High-alpha handling qualities flight research on the NASA F/A-18 High Alpha Research Vehicle [microform] / Keith D. Wichman ... [et al.].

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1996.
    • 1996
  • Airfoil dynamic stall and rotorcraft maneuverability [microform] / William G. Bousman.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information, [2000]
    • 2000
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS23428
  • Candidate control design metrics for an agile fighter [microform] / Patrick C. Murphy, Melvin L. Bailey, Aaron J. Ostroff.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1991.
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60321
  • Subsonic flow investigations on a cranked wing designed for high maneuverability / Dhanvada M. Rao.

    • Text
    • Hampton, Va. : Vigyan Research Associates, Inc. : National Aeronautics and Space Administration, Langley Research Center, [1986]
    • 1986
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo27947
  • Subsonic flow investigations on a cranked wing designed for high maneuverability [microform] / Dhanvada M. Rao.

    • Text
    • Hampton, Va. : Vigyan Research Associates, Inc. : National Aeronautics and Space Administration, Langley Research Center, [1986]
    • 1986
  • Structural dynamic model obtained from flight for use with piloted simulation and handling qualities analysis / Bruce G. Powers.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, June 1996.
    • 1996-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65385
  • High-Alpha handling qualities flight research on the NASA F/A-18 High Alpha Research Vehicle / Keith D. Wichman [and six others]

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, November 1996.
    • 1996-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65674
  • Economic evaluation of flying-qualities design criteria for a transport configured with relaxed static stability / Steven M. Sliwa.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
    • 1980-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71360
  • Airfoil dynamic stall and rotorcraft maneuverability / William G. Bousman.

    • Text
    • Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, July 2000.
    • 2000-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS23428
  • Semi-annual status report on NASA grant NAG 1-1087 : "identification of aerodynamic models for maneuvering aircraft" / by Suei Chin and C. Edward Lan.

    • Text
    • Lawrence, Kan. : Flight Research Laboratory, The University of Kansas Center for Research, Inc., [1990]
    • 1990
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS60899

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