Research Catalog

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  • Vehicle integration effects on hypersonic waveriders [microform] / Charles Edward Cockrell, Jr.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Lateral stability analysis for X-29A drop model using system identification methodology [microform] / David L. Raney and James G. Batterson.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1989.
    • 1989

  • Controls design with crossfeeds for hovering rotcract using quantitative feedback theory [microform] / by Daniel J. Biezad.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Low-speed wind tunnel tests of two waverider configuration models [microform] / Robert J. Pegg, David E. Hahne, Charles E. Cockrell, Jr.

    • Text
    • Washington, D.C. : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • A computational examination of directional stability for smooth and chined forebodies at High-α [microform] / Ramakrishnan Ravi and William H. Mason.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1992.
    • 1992

  • Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack [microform] / Kenneth W. Iliff, Kon-Sheng Charles Wang.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1997.
    • 1997

  • Flight-determined, subsonic, lateral-directional stability and control derivatives of the thrust-vectoring F-18 high angle of attack research vehicle (HARV), and comparisons to the basic F-18 and predicted derivates [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, [1999]
    • 1999

  • X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data [microform] / Kenneth W. Iliff, Kon-Sheng Charles Wang.

    • 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

  • Hi-alpha forebody design [microform] / by William H. Mason and R. Ravi.

    • Text
    • Blacksburg, VA : Dept. of Aerospace and Ocean Engineering, Virginia Polytechnic Institute and State University ; [Washington, DC : National Aeronautics and Space Administration, 1992-
    • 1992-present

  • Low-speed static and dynamic force tests of a generic supersonic cruise fighter configuration [microform] / David E. Hahne.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989.
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS97104

  • Application and evaluation of control modes for risk-based engine performance enhancements / Yuan Liu [and four others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, January 2015.
    • 2015-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo57885

  • Experimental aerodynamic characteristics of the Pegasus air-launched booster and comparisons with predicted and flight results / M.N. Rhode and W.C. Engelund, M.R. Mendenhall.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [1995]
    • 1995
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo77772

  • Experimental aerodynamic characteristics of the Pegasus air-launched booster and comparisons with predicted and flight results / M.N. Rhode and W.C. Engelund, M.R. Mendenhall.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [1995]
    • 1995

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