Research Catalog

  • A flying qualities study of longitudinal long-term dynamics of hypersonic planes [microform] / Timothy H. Cox ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor], 1995.
    • 1995
  • Modeling of longitudinal unsteady aerodynamics of a wing-tail combination [microform] / Vladislav Klein.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999
  • Cg/stability map for the reference H cycle 3 supersonic transport concept along the high speed research baseline mission profile [microform] / Daniel P. Giesy and David M. Christhilf.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999
  • Development of flight testing techniques [microform] : final report, 10/31/79 - 10/31/84 / principal investigator, Doral R. Sandlin.

    • Text
    • San Luis Obispo, CA : Aeronautical Engineering Dept., California Polytechnic State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1984]
    • 1984
  • Low-speed wind tunnel study of longitudinal stability and usable-lift improvement of a cranked wing [microform] / Dhanvada M. Rao.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1987]
    • 1987
  • Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept [microform] / A.M. Springer.

    • Text
    • MSFC, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Reduction of Blade-Vortex Interaction (BVI) noise through X-force control [microform] / Fredric H. Schmitz.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration [microform] / W.P. Phillips and W.C. Engelund.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997
  • Euler/Navier-Stokes flow computations on flexible configurations for stability analysis [microform] / G. Guruswamy and E. Tu.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, American Institute of Aeronautics and Astronautics ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1995
  • Development of three-dimensional flow code package to predict performance and stability of aircraft with leading edge ice contamination [microform] / D.J. Strash and J.M. Summa.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring [microform] / Kenneth W. Iliff, Kon-Sheng Charles Wang.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997
  • Locally linearized longitudinal and lateral-directional aerodynamic stability and control derivaties for the X-29A aircraft [microform] / Gerald D. Budd.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [Springfield, Va. : For sale by the National Technical Information Service, 1984]
    • 1984
  • Longitudinal aerodynamic characteristics of a subsonic, energy-efficient transport configuration in the National Transonic Facility [microform] / Peter F. Jacobs and Blair B. Gloss.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67806
  • Summary of longitudinal stability and control parameters as determined from space shuttle Challenger flight test data [microform] / William T. Suit.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, VA : For sale by the National Technical Information Service, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS93085
  • Comparison of Space Shuttle Orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests / Delma C. Freeman, Jr., and Barnard Spencer, Jr.

    • 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/gpo71431
  • A flying qualities study of longitudinal long-term dynamics of hypersonic planes / Timothy H. Cox [and three others].

    • Text
    • Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Facility, April 1995.
    • 1995-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo82735

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