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  1. 1
    Wind tunnel measurements in the wakes of structures

    Wind tunnel measurements in the wakes of structures by Woo, H. G. 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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  2. 2
    Installation and test of Doppler acoustic sensor

    Installation and test of Doppler acoustic sensor by McConville, R P.

    Washington : Springfield, Va. : Dept. of Transportation, Federal Aviation Administration, Systems Research and Development Service ; For sale by the National Technical Information Service, 1977
    Format: Government Document Book


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  3. 3
    Application of a panel method to wake-vortex/wing interaction and comparison with experimental data

    Application of a panel method to wake-vortex/wing interaction and comparison with experimental data by Smith, Brian E.

    Moffett Field, Calif. : Springfield, Va. : National Aeronautics and Space Administration, Ames Research Center ; For sale by the National Technical Information Service, 1987
    Format: Government Document Book


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  4. 4
    A comparison of airborne wake vortex detection measurements with values predicted from potential theory

    A comparison of airborne wake vortex detection measurements with values predicted from potential theory by Stewart, Eric C.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [For sale by the National Technical Information Service], 1991
    Format: Government Document Book


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  5. 5
    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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  6. 6
    Aircraft propeller induced structure-borne noise

    Aircraft propeller induced structure-borne noise by Unruh, James F.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1989
    Format: Government Document Book


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  7. 7
    Development of an unsteady wake theory appropriate for aeroelastic analyses of rotors in hover and forward flight first semi-annual status report

    Development of an unsteady wake theory appropriate for aeroelastic analyses of rotors in hover and forward flight first semi-annual status report by Peters, D. A.

    Atlanta, Ga. : School of Aerospace Engineering, Georgia Institute of Technology, 1988
    Format: Government Document Book


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  8. 8
    Hypersonic rarefied wake characterization

    Hypersonic rarefied wake characterization by Brewer, E. B.

    [Washington, DC] : [Springfield, Va. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; For sale by the National Technical Information Service], 1993
    Format: Government Document Book


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  9. 9
    Vortex advisory system safety analysis

    Vortex advisory system safety analysis by Hallock, J. N. (James N.)

    Washington, DC : Springfield, Va. : The Service ; National Technical Information Service [distributor], 1978
    Format: Government Document Book


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  10. 10
    Wake vortex minimization : a symposium held at Washington, D.C., on February 25-26, 1976.

    Wake vortex minimization : a symposium held at Washington, D.C., on February 25-26, 1976.

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


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  11. 11
    Wake turbulence training aid : final report.

    Wake turbulence training aid : final report.

    [Washington, DC] : [Springfield, Va.] : U.S. Dept. of Transportation, Federal Aviation Administration ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  12. 12
    Analysis of noise measured from a propeller in a wake

    Analysis of noise measured from a propeller in a wake by Block, P. J. W.

    [Washington, D.C.?] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1984
    Format: Government Document Book


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  13. 13
    Hypersonic rarefied wake characterization

    Hypersonic rarefied wake characterization by Brewer, E. B.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [For sale by the National Technical Information Service], 1993
    Format: Government Document Book


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  14. 14
    Helicopter rotor wake geometry and its influence in forward flight

    Helicopter rotor wake geometry and its influence in forward flight by Egolf, T. Alan

    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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  15. 15
    Periodic vortex shedding in the supersonic wake of a planar plate

    Periodic vortex shedding in the supersonic wake of a planar plate by Xing, W. F.

    Washington DC : National Aeronautics and Space Administration, 1985
    Format: Government Document Book


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  16. 16
    Prediction of subsonic vortex shedding from forebodies with chines

    Prediction of subsonic vortex shedding from forebodies with chines by Mendenhall, M. R.

    [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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  17. 17
    Laminar wakes

    Laminar wakes by Berger, Stanley A., 1934-2013

    New York : American Elsevier Pub. Co., 1971
    Format: Book


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  18. 18
    Application of a panel method to wake-vortex/wing interaction and comparison with experimental data

    Application of a panel method to wake-vortex/wing interaction and comparison with experimental data by Smith, Brian E.

    Moffett Field, Calif. : Springfield, Va. : National Aeronautics and Space Administration, Ames Research Center ; For sale by the National Technical Information Service, 1987
    Format: Government Document Book


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  19. 19
    Application of FAA wake vortex research to safety : hearing before the Subcommittee on Technology, Environment, and Aviation of the Committee on Science, Space, and Technology, U.S. House of Representatives, One Hundred Third Congress, second session, July 28, 1994.

    Application of FAA wake vortex research to safety : hearing before the Subcommittee on Technology, Environment, and Aviation of the Committee on Science, Space, and Technology, U.S...

    Washington : U.S. G.P.O. : For sale by the U.S. G.P.O., Supt. of Docs., Congressional Sales Office, 1995
    Format: Government Document Book


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  20. 20
    Wake characteristics of an eight-leg tower for a MOD-O type wind turbine

    Wake characteristics of an eight-leg tower for a MOD-O type wind turbine by Savino, J. M.

    Cleveland, Ohio : Springfield, Va. : National Aeronautics and Space Administration, Lewis Research Center ; For sale by the National Technical Information Service, 1977
    Format: Government Document Book


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