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  1. 1
    Wind tunnel results of the aerodynamic performance of a 1/8-scale model of a twin-engine transport with multi-element wing

    Wind tunnel results of the aerodynamic performance of a 1/8-scale model of a twin-engine transport with multi-element wing

    Hampton, Va. : [Springfield, Va.] :; 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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  2. 2
    Validation of vortex-lattice method for loads on wings in lift-generated wakes

    Validation of vortex-lattice method for loads on wings in lift-generated wakes by Rossow, Vernon J.

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


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  3. 3
    Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges

    Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges by Chu, Julio

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1996
    Format: Government Document Book


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  4. 4
    Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds

    Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds

    Hampton, Va. : Hanover Md. :; Hampton, Va. : Hanover MD : National Aeronautics and Space Administration, Langley Research Center ; Available from NASA Center for AeroSpace Information (CASI), 2001
    Format: Government Document Book


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  5. 5
    Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration

    Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration by Phillips, W. Pelham

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1997
    Format: Government Document Book


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  6. 6
    Noise exposure reduction of advanced high-lift systems

    Noise exposure reduction of advanced high-lift systems by Haffner, Stephen W.

    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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  7. 7
    Highlights of aeroacoustics research in the U.S.-1998

    Highlights of aeroacoustics research in the U.S.-1998 by Raman, Ganesh

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


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  8. 8
    The development of a highly reliable power management and distribution system for civil transport aircraft

    The development of a highly reliable power management and distribution system for civil transport aircraft by Coleman, Anthony S.

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


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  9. 9
    Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ̊angle of attack : contract NAS 3-26617

    Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ̊angle of attack : contract NAS 3-26617

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


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  10. 10
    Low-speed wind tunnel tests of two waverider configuration models

    Low-speed wind tunnel tests of two waverider configuration models by Pegg, Robert J.

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


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  11. 11
    Aeroacoustic effects of reduced aft tip speed at constant thrust for a model counterrotation turboprop at takeoff conditions

    Aeroacoustic effects of reduced aft tip speed at constant thrust for a model counterrotation turboprop at takeoff conditions by Woodward, Richard P.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1990
    Format: Government Document Book


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  12. 12
    A general theory of two-and three-dimensional rotational flow in subsonic and transonic turbomachines

    A general theory of two-and three-dimensional rotational flow in subsonic and transonic turbomachines by Wu, Zuxiang

    [Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1993
    Format: Government Document Book


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  13. 13
    Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft

    Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft

    Edwards, Calif. : Springfield, VA :; Edwards, Calif. : Springfield, VA : National Aeronautics and Space Administration, Dryden Flight Research Center ; National Technical Information Service, distributor, 1999
    Format: Government Document Book


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  14. 14
    Ultra-high bypass ratio jet noise

    Ultra-high bypass ratio jet noise by Low, John K. C.

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


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  15. 15
    Design of supersonic transport flap systems for thrust recovery at subsonic speeds

    Design of supersonic transport flap systems for thrust recovery at subsonic speeds by Mann, Michael J.

    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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  16. 16
    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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  17. 17
    Noise impact of advanced high lift systems : contract NAS1-20103

    Noise impact of advanced high lift systems : contract NAS1-20103 by Elmer, Kevin R.

    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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  18. 18
    Numerical study to assess sulfur hexafluoride as a medium for testing multielement airfoils

    Numerical study to assess sulfur hexafluoride as a medium for testing multielement airfoils by Bonhaus, Daryl L.

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


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  19. 19
    Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept

    Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept by Springer, A. M.

    MSFC, Ala. : [Springfield, Va.] : National Aeronautics and Space Administration, Marshall Space Flight Center ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  20. 20
    Effect of passive venting on static pressure distributions in cavities at subsonic and transonic speeds

    Effect of passive venting on static pressure distributions in cavities at subsonic and transonic speeds

    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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