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  1. 1
    Investigations of detail design issues for the high speed acoustic wind tunnel using a 60th scale model tunnel : final report

    Investigations of detail design issues for the high speed acoustic wind tunnel using a 60th scale model tunnel : final report by Bama, P. S.

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1991
    Format: Government Document Book


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  2. 2
    Modeling the benchmark active control technology wind-tunnel model for active control design applications

    Modeling the benchmark active control technology wind-tunnel model for active control design applications by Waszak, Martin R.

    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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  3. 3
    Dynamic response tests of inertial and optical wind-tunnel model attitude measurement devices

    Dynamic response tests of inertial and optical wind-tunnel model attitude measurement devices

    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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  4. 4
    Uncertainty analysis of inertial model attitude sensor calibration and application with a recommended new calibration method

    Uncertainty analysis of inertial model attitude sensor calibration and application with a recommended new calibration method by Tripp, John S.

    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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  5. 5
    Stereo electro-optical tracking system (SETS)

    Stereo electro-optical tracking system (SETS) by Koenig, Edward W.

    Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1984
    Format: Government Document Book


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  6. 6
    Effect of contact surface bluntness on massive blowing from a wedge in hypersonic flow.

    Effect of contact surface bluntness on massive blowing from a wedge in hypersonic flow.

    Ft. Belvoir Defense Technical Information Center 1966
    Format: Government Document Book


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  7. 7
    A systematic plan for the continued study of dimensional stability of metallic alloys considered for the fabrication of cryogenic wind tunnel models

    A systematic plan for the continued study of dimensional stability of metallic alloys considered for the fabrication of cryogenic wind tunnel models by Wigley, D. A.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1985
    Format: Government Document Book


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  8. 8
    Remote sensing of hydrologic variables in boreal areas

    Remote sensing of hydrologic variables in boreal areas by Peck, Eugene L.

    [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
    Recommended practice : calibration of subsonic and transonic wind tunnels.

    Recommended practice : calibration of subsonic and transonic wind tunnels.

    Reston, Va. : American Institute of Aeronautics and Astronautics, 2003
    Format: Book


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  10. 10
    Roll-yaw control at high angle of attack by forebody tangential blowing

    Roll-yaw control at high angle of attack by forebody tangential blowing

    [Stanford, Calif.?] : [Washington, DC] : [Springfield, Va.] : Joint Institute for Aeronautics and Acoustics ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  11. 11
    Using transonic small disturbance theory for predicting the aeroelastic stability of a flexible wind-tunnel model

    Using transonic small disturbance theory for predicting the aeroelastic stability of a flexible wind-tunnel model by Silva, Walter A.

    Hampton, Va. :; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1990
    Format: Government Document Book


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  12. 12
    A systematic plan for the continued study of dimensional stability of metallic alloys considered for the fabrication of cryogenic wind tunnel models

    A systematic plan for the continued study of dimensional stability of metallic alloys considered for the fabrication of cryogenic wind tunnel models by Wigley, D. A.

    Hampton, Va. : [Springfield, Va. : National Aeronautics and Space Administration, Langley Research Center ; For sale by the National Technical Information Service, 1985
    Format: Government Document Book


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  13. 13
    Description of panel method code ANTARES

    Description of panel method code ANTARES by Ulbrich, Norbert

    Moffett, Field, Calif. : Hanover, Md. : National Aeronautics and Space Administration, Ames Research Center ; Available from NASA Center for Aerospace Information, 2000
    Format: Government Document Book


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  14. 14
    Aeroelasticity and mechanical stability report, 0.27 mach scale model of the YAH-64 advanced attack helicopter

    Aeroelasticity and mechanical stability report, 0.27 mach scale model of the YAH-64 advanced attack helicopter by Straub, F. K.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1987
    Format: Government Document Book


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  15. 15
    A comparison of pressure measurements between a full-scale and a 1/6-scale F/A-18 twin tail during buffet

    A comparison of pressure measurements between a full-scale and a 1/6-scale F/A-18 twin tail during buffet by Moses, Robert W.

    Hampton, Va. : [Springfield, Va.] :; 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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  16. 16
    Experimental evaluation of two turning vane designs for high-speed corner of 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel

    Experimental evaluation of two turning vane designs for high-speed corner of 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel by Moore, Royce D.

    [Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1986
    Format: Government Document Book


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  17. 17
    Development of a model protection and dynamic response monitoring system for the National Transonic Facility

    Development of a model protection and dynamic response monitoring system for the National Transonic Facility by Young, Clarence P.

    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
    The Wind Tunnel Model : transdisciplinary encounters

    The Wind Tunnel Model : transdisciplinary encounters by Dombois, Florian, 1966-

    Zurich : Scheidegger & Spiess, 2017
    Format: Book


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  19. 19
    The Wind tunnel model surface gauge for measuring roughness

    The Wind tunnel model surface gauge for measuring roughness

    [Gaithersburg, MD. : U.S. Dept. of Commerce, National Bureau of Standards, 1987
    Format: Government Document Book


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  20. 20
    Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel : report on the modified D.S.M.A. design

    Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel : report on the modified D.S.M.A. design by Barna, P. S.

    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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