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  • Development of a mulicomponent force and moment balance for water tunnel applications [microform] / Carlos J. Suárez ... [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], 1994.
    • 1994

  • Effects of yaw and pitch motion on model attitude measurements [microform] / Ping Tcheng, John S. Tripp, and Tom D. Finley.

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

  • Helicopter low-speed yaw control [microform] / inventors, John C. Wilson, Henry L. Kelley, Cynthia A. Crowell.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • Feedback control laws for highly maneuverable aircraft [microform] / by William L. Garrard and Gary J. Balas.

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

  • Evaluation of F/A-18A HARV inlet flow analysis with flight data [microform] / C. Frederic Smith ... [et al.].

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Calibration of the NASA Lewis Research Center 9- by 15-foot low speed wind tunnel (1994 test) [microform] / E. Allen Arrington and Jose C. Gonsalez.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Experiments in aircraft roll-yaw control using forebody tangential blowing [microform] / Nelson Pedreiro.

    • Text
    • [Stanford, Calif.] : Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center : Joint Institute for Aeronautics and Acoustics, Stanford University ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • A parametric study of accelerations of an airplane due to a wake vortex system [microform] / Eric C. Stewart.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • Semicoarsening and implicit smoothers for the simulation of a flat plate at yaw [microform] / Ruben S. Montero and Ignacio M. Llorente, Manuel D. Salas ; prepared for Langley Research Center under contract NAS1-97046.

    • Text
    • Hampton, VA : ICASE, NASA Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001

  • Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes [microform] / Robert J. Foley, Odis C. Pendergraft, Jr.

    • 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

  • Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles [microform] / Mary L. Mason and Bobby L. Berrier.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985.
    • 1985

  • Progress in multirate digital control system design [microform] / Martin C. Berg and Gregory S. Mason.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center : [Springfield, Va. : For sale by the National Technical Information Service, 1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS59875

  • Determination of shuttle orbiter center of gravity from flight measurements [microform] / E. W. Hinson, J. Y. Nicholson, R. C. Blanchard.

    • Text
    • Hampton, Va. : NASA Langley Research Center, [1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60549

  • Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds [microform] / E.B. Plentovich, Julio Chu, and M.B. Tracy.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67795

  • An investigation of the use of bandwidth criteria for rotorcraft handling-qualities specifications [microform] / Chris L. Blanken, Courtland C. Bivens, and Matthew S. Whalley.

    • Text
    • Moffett Field, Calif. : Aeromechanics Laboratory, U.S. Army Research and Technology Laboratories (AVSCOM), NASA Ames Research Center, [1985]
    • 1985

  • ADDJUST : a view of the first 25 years / Joe Nieberding and Craig H. Williams.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, May 2015.
    • 2015-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo59881

  • Flight simulator evaluation of enhanced propulsion control modes for emergency operation / Jonathan S. Litt [and four others].

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo37876

  • Methods for estimating stability and control derivatives of conventional subsonic airplanes.

    • Text
    • [Lawrence? Kan.], [1971]
    • 1971
    • 1 Item
    FormatCall NumberItem Location
    Text TL574.S7R57Off-site

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