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  • Why do airlines want and use thrust reversers? [microform] : a compilation of airline industry responses to a survey regarding the use of thrust reversers on commercial transport planes / J. A. Yetter.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows [microform] / by Scott T. Imlay.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service, 1986.
    • 1986

  • Investigation of wing upper surface flow-field disturbance due to NASA DC-8-72 in-flight inboard thrust-reverser deployment [microform] / Hedayat U. Hamid, Richard J. Margason, and Gordon Hardy.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Magellan aerodynamic characteristics during the termination experiment including thruster plume-free stream interaction [microform] : under cooperative agreement NCC1-104 / Francisco J. Cestero and Robert H. Tolson.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Static performance of six innovative thrust reverser concepts for subsonic transport applications [microform] : summary of the NASA Langley Innovative Thrust Reverser Test Program / Scott C. Asbury and Jeffrey A. Yetter.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information (CASI), [2000]
    • 2000
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS22791

  • Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap [microform] / Richard J. Re and Laurence D. Leavitt.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986.
    • 1986

  • Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability [microform] / Linda S. Bangert and Laurence D. Leavitt.

    • 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/LPS60139

  • Full-scale thrust reverser testing in an altitude facility [microform] / Charles M. Mehalic and Roy A. Lottig.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1987]
    • 1987
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS92432

  • Measured pressure distributions inside nonaxisymmetric nozzles with partially deployed thrust reversers / Robert S. Green, George T. Carson, Jr.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
    • 1987
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS112156

  • Measured pressure distributions inside nonaxisymmetric nozzles with partially deployed thrust reversers [microform] / Robert S. Green, George T. Carson, Jr.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
    • 1987
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS112156

  • An investigation at static conditions of nonaxisymmetric nozzle thrust reverser port geometry including effects of rounding and rotating the port corner [microform] / Dorothy G. Arbiter.

    • Text
    • Hampton, Va. : Vigyan Research Associates, Inc. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985

  • Static performance of six innovative thrust reverser concepts for subsonic transport applications : summary of the NASA Langley Innovative Thrust Reverser Test Program / Scott C. Asbury and Jeffrey A. Yetter.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, July 2000.
    • 2000-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS22791

  • Plasma actuators for turbomachinery flow control, final report / Richard B. Miles and Mikhail N. Shneider.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo33409

  • Preliminary experiments on the noise generated by target-type thrust reverser models / by Orlando A. Gutierrez and James R. Stone.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, May 1972.
    • 1972-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo173326

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