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  1. 1
    Computer-aided light sheet flow visualization using photogrammetry

    Computer-aided light sheet flow visualization using photogrammetry by Stacy, Kathryn

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1994
    Format: Government Document Book


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  2. 2
    Development and implementation of software for visualizing and editing multidimensional flight simulation input data : a thesis ...

    Development and implementation of software for visualizing and editing multidimensional flight simulation input data : a thesis ... by Whelan, Todd Michael

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1996
    Format: Government Document Book


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  3. 3
    Low-order nonlinear dynamic model of IC engine-variable pitch propeller system for general aviation aircraft

    Low-order nonlinear dynamic model of IC engine-variable pitch propeller system for general aviation aircraft by Richard, Jacques C.

    [Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  4. 4
    NASA Dryden Flow Visualization Facility

    NASA Dryden Flow Visualization Facility by Del Frate, John H.

    [Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  5. 5
    Fourier functional analysis for unsteady aerodynamic modeling

    Fourier functional analysis for unsteady aerodynamic modeling by Chin, Suei

    Lawrence, Kan. : [Washington, D.C.] :; Lawrence, Kan. : [Washington, D.C. :] : Flight Research Laboratory, University of Kansas Center for Research ; [National Aeronautics and Space Administration], 1991
    Format: Government Document Book


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  6. 6
    Structural dynamic model obtained from flight use with piloted simulation and handling qualities analysis

    Structural dynamic model obtained from flight use with piloted simulation and handling qualities analysis by Powers, Bruce G.

    [Washington, D.C.] : [Springfield, Va.] :; [Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1996
    Format: Government Document Book


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  7. 7
    An evaluation technique for an F/A-18 aircraft loads model using F/A-18 systems research aircraft flight data

    An evaluation technique for an F/A-18 aircraft loads model using F/A-18 systems research aircraft flight data by Brenner, Marty, 1955-

    Edwards, Calif. : Hanover, MD : National Aeronautics and Space Administration, Dryden Flight Research Center ; Available from NASA Center for AeroSpace Information (CASI), 2000
    Format: Government Document Book


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  8. 8
    High speed civil transport aircraft simulation : reference-H cycle 1 : MATLAB implementation

    High speed civil transport aircraft simulation : reference-H cycle 1 : MATLAB implementation by Sotack, Robert A.

    Hampton, Va. : Springfield, Va. : National Aeronautics and Space Administration, Langley Research Center ; Available from National Technical Information Service, 1999
    Format: Government Document Book


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  9. 9
    Controls design with crossfeeds for hovering rotorcraft using quantitative feedback theory

    Controls design with crossfeeds for hovering rotorcraft using quantitative feedback theory by Biezad, Daniel J.

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1994
    Format: Government Document Book


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  10. 10
    Derivation and definition of a linear aircraft model

    Derivation and definition of a linear aircraft model by Duke, Eugene L.

    [Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1988
    Format: Government Document Book


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  11. 11
    Radial and circumferential flow surveys at the inlet and exit of the Space Shuttle Main Engine High Pressure Fuel Turbine model

    Radial and circumferential flow surveys at the inlet and exit of the Space Shuttle Main Engine High Pressure Fuel Turbine model

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  12. 12
    Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane

    Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane by Allison, Dennis O.

    Hampton, Va. : Springfield, VA : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service (NTIS) [distributor], 1995
    Format: Government Document Book


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  13. 13
    Generic airplane model concept and four specific models developed for use in piloted simulation studies

    Generic airplane model concept and four specific models developed for use in piloted simulation studies by Hoffler, Keith D.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1997
    Format: Government Document Book


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  14. 14
    Electromagnetic on-aircraft antenna radiation in the presence of composite plates

    Electromagnetic on-aircraft antenna radiation in the presence of composite plates by Kan, S. H-T

    Columbus, Ohio : Hampton, VA : Springfield, Va. : The Ohio State University, ElectroScience Laboratory, Dept. of Electrical Engineering ; National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor, 1994
    Format: Government Document Book


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  15. 15
    Numerical stability and control analysis towards falling-leaf prediction capabilities of splitflow for two generic high-performance aircraft models

    Numerical stability and control analysis towards falling-leaf prediction capabilities of splitflow for two generic high-performance aircraft models by Charlton, Eric F.

    Hampton, Va. : Springfield, VA : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor, 1998
    Format: Government Document Book


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  16. 16
    Acoustic treatment design scaling methods.

    Acoustic treatment design scaling methods. by Kraft, R. E. (Robert Eugene)

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1999
    Format: Government Document Book


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  17. 17
    STOVL Control Integration Program

    STOVL Control Integration Program by Weiss, Karl, 1738-1795

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1994
    Format: Government Document Book


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  18. 18
    Nonlinear axisymmetric and three-dimensional vorticity dynamics in a swirling jet model

    Nonlinear axisymmetric and three-dimensional vorticity dynamics in a swirling jet model by Martin, J. E.

    Hampton, Va. : [Springfield, Va.] : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [National Technical Information Service, distributor], 1997
    Format: Government Document Book


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  19. 19
    Integrated Advanced Microwave Sounding Unit-A (AMSU-A), performance verification report, METSAT Phase Locked Oscillator assembly, P/N 1348360-1, S/N's F07 and F08 : contract no. NAS 5-32314

    Integrated Advanced Microwave Sounding Unit-A (AMSU-A), performance verification report, METSAT Phase Locked Oscillator assembly, P/N 1348360-1, S/N's F07 and F08 : contract no. NA... by Pines, D.

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1998
    Format: Government Document Book


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  20. 20
    Effects of yaw and pitch motion on model attitude measurements

    Effects of yaw and pitch motion on model attitude measurements by Tcheng, Ping

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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