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  1. 1
    Effects of perforated flap surfaces and screens on acoustics of a large externally blown flap model

    Effects of perforated flap surfaces and screens on acoustics of a large externally blown flap model by Burns, Robert J.

    Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1976
    Format: Government Document Book


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  2. 2
    Aircraft accident report : Northwest Airlines, Inc., McDonnell Douglas DC-9-82, N312RC, Detroit Metropolitan Wayne County Airport, Romulus, Michigan, August 16, 1987

    Aircraft accident report : Northwest Airlines, Inc., McDonnell Douglas DC-9-82, N312RC, Detroit Metropolitan Wayne County Airport, Romulus, Michigan, August 16, 1987

    Washington, D.C. : [Springfield, Va. : The Board ; National Technical Information Service, distributor, 1988
    Format: Government Document Book


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  3. 3
    Military airlift : C-17 flap requires additional testing : statement for the record by Nancy R. Kingsbury, Director, Air Force Issues, National Security and International Affairs Division, before the Legislation and National Security Subcommittee, Committee on Government Operations, House of Representatives

    Military airlift : C-17 flap requires additional testing : statement for the record by Nancy R. Kingsbury, Director, Air Force Issues, National Security and International Affairs D... by Kingsbury, Nancy R.

    Washington, D.C. : Gaithersburg, MD (P.O. Box 6015, Gaithersburg 20877) : The Office ; The Office [distributor], 1992
    Format: Government Document Book


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  4. 4
    Wake profile measurements of fixed and oscillating flaps

    Wake profile measurements of fixed and oscillating flaps by Owen, F. Kevin

    Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, 1984
    Format: Government Document Book


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  5. 5
    Initial piloted simulation study of geared flap control for tilt-wing V/STOL aircraft

    Initial piloted simulation study of geared flap control for tilt-wing V/STOL aircraft by Guerrero, Lourdes M.

    Moffett Field, Calif. : [Springfield, Va.] : National Aeronautics and Space Administration, Ames Research Center ; [For sale by the National Technical Information Service], 1991
    Format: Government Document Book


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  6. 6
    Validation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application of optimization

    Validation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application of optimizatio... by Carlson, Harry W.

    [Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1990
    Format: Government Document Book


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  7. 7
    Aeroacoustic performance of an externally blown flap configuration with several flap noise suppression devices

    Aeroacoustic performance of an externally blown flap configuration with several flap noise suppression devices by McKinzie, Daniel J.

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982
    Format: Government Document Book


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  8. 8
    Flight control system development and flight test experience with the F-111 mission adaptive wing aircraft

    Flight control system development and flight test experience with the F-111 mission adaptive wing aircraft by Larson, Richard R.

    Edwards, Calif. : [Springfield, Va.] : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [For sale by the National Technical Information Service], 1986
    Format: Government Document Book


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  9. 9
    Blade-mounted trailing edge flap control for BVI noise reduction

    Blade-mounted trailing edge flap control for BVI noise reduction

    [Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1992
    Format: Government Document Book


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  10. 10
    Subsonic wind-tunnel measurements of a slender wing-body configuration employing a vortex flap

    Subsonic wind-tunnel measurements of a slender wing-body configuration employing a vortex flap by Frink, Neal T.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1987
    Format: Government Document Book


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  11. 11
    A comparison of the results of dynamic wind-tunnel test with theoretical predictions for an aeromechanical gust-alleviation system for light airplanes

    A comparison of the results of dynamic wind-tunnel test with theoretical predictions for an aeromechanical gust-alleviation system for light airplanes by Stewart, Eric C.

    Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977
    Format: Government Document Book


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  12. 12
    Calculation of the longitudinal aerodynamic characteristics of upper-surface blown wing-flap configurations

    Calculation of the longitudinal aerodynamic characteristics of upper-surface blown wing-flap configurations by Mendenhall, M. R.

    Washington : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978
    Format: Government Document Book


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  13. 13
    Flap effectiveness on subsonic longitudinal aerodynamic characteristics of a modified arrow wing

    Flap effectiveness on subsonic longitudinal aerodynamic characteristics of a modified arrow wing by Quinto, P. Frank

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1983
    Format: Government Document Book


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  14. 14
    Validation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application of optimization

    Validation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application of optimizatio... by Carlson, Harry W.

    [Washington, D.C.] : [Springfield, Va. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; For sale by the National Technical Information Service], 1990
    Format: Government Document Book


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  15. 15
    Flow-field measurements on an airfoil with an oscillating trailing-edge flap using holographic interferometry

    Flow-field measurements on an airfoil with an oscillating trailing-edge flap using holographic interferometry by Bachalo, W. D.

    Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, 1984
    Format: Government Document Book


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  16. 16
    Subsonic wind-tunnel measurements of a slender wing-body configuration employing a vortex flap

    Subsonic wind-tunnel measurements of a slender wing-body configuration employing a vortex flap by Frink, Neal T.

    [Washington, DC] : [Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service], 1987
    Format: Government Document Book


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  17. 17
    Aircraft accident report : Empire Airlines flight 141, Piper PA-31, N546BA, Ithaca, New York, January 5, 1982

    Aircraft accident report : Empire Airlines flight 141, Piper PA-31, N546BA, Ithaca, New York, January 5, 1982

    Washington, D.C. : Springfield, Va. : The Board ; [National Technical Information Service, distributor], 1982
    Format: Government Document Book


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  18. 18
    Low-speed investigation of effects of wing leading- and trailing-edge flap deflections and canard incidence on a fighter configuration equipped with a forward-swept wing

    Low-speed investigation of effects of wing leading- and trailing-edge flap deflections and canard incidence on a fighter configuration equipped with a forward-swept wing by Gainer, Thomas G.

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1984
    Format: Government Document Book


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  19. 19
    A method for calculating externally blown flap noise

    A method for calculating externally blown flap noise by Fink, Martin R.

    [Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information, 1978
    Format: Government Document Book


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  20. 20
    Investigation of trailing-edge-flap spanwise-blowing concepts on an advanced fighter configuration

    Investigation of trailing-edge-flap spanwise-blowing concepts on an advanced fighter configuration by Paulson, John W.

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1984
    Format: Government Document Book


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