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  1. 1
    Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel

    Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel by Schuster, D. M. (David M.)

    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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  2. 2
    Flow through a rectangular-to-semiannular diffusing transition duct

    Flow through a rectangular-to-semiannular diffusing transition duct

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


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  3. 3
    Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel

    Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel by Plentovich, Elizabeth B.

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


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  4. 4
    Evaluation of F/A-18A HARV inlet flow analysis with flight data

    Evaluation of F/A-18A HARV inlet flow analysis with flight data

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


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  5. 5
    A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92

    A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92 by Re, Richard J.

    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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  6. 6
    Rocket-based combined cycle engine technology development : inlet CFD validation and application

    Rocket-based combined cycle engine technology development : inlet CFD validation and application by DeBonis, James R.

    [Cleveland, Ohio] : [Springfield, Va.] :; [Cleveland, Ohio] : [Springfield, Va.] : National Aeronautics and Space Administration, Lewis Research Center, Ohio Aerospace Institute, Institute for Computational Mechanics in Propulsion ; [National Aeronautics and Space Administration, distributor], 1996
    Format: Government Document Book


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  7. 7
    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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  8. 8
    PSP measurement of stator vane surface pressures in a high speed fan

    PSP measurement of stator vane surface pressures in a high speed fan by Lepicovsky, Jan

    [Cleveland, Ohio] : [Springfield, Va.] : National Aeronautics and Space Administration, Lewis Research Center ; [National Technical Information Service, distributor], 1998
    Format: Government Document Book


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  9. 9
    The application to airfoils of a technique for reducing orifice-induced pressure error at high Reynolds numbers

    The application to airfoils of a technique for reducing orifice-induced pressure error at high Reynolds numbers by Plentovich, Elizabeth B.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [National Technical Information Service, distributor], 1986
    Format: Government Document Book


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  10. 10
    Calibration of the NASA Lewis Research Center 9- by 15-foot low speed wind tunnel (1994 test)

    Calibration of the NASA Lewis Research Center 9- by 15-foot low speed wind tunnel (1994 test) by Arrington, E. Allen

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


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  11. 11
    A preliminary look at techniques used to obtain airdata from flight at high angles of attack

    A preliminary look at techniques used to obtain airdata from flight at high angles of attack by Moes, Timothy R.

    Edwards, Calif. : [Springfield, Va.] : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [National Technical Information Service, distributor], 1990
    Format: Government Document Book


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  12. 12
    Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel

    Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel by Re, Richard, J.

    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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  13. 13
    Experimental investigation of crossing shock wave-turbulent boundary layer-bleed interaction

    Experimental investigation of crossing shock wave-turbulent boundary layer-bleed interaction by Kim, Hyun Dae

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


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  14. 14
    Study of CFD methods applied to rapidly deforming boundaries

    Study of CFD methods applied to rapidly deforming boundaries by Slater, John W.

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


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  15. 15
    Estimating engine airflow in gas-turbine powered aircraft with clean and distorted inlet flows

    Estimating engine airflow in gas-turbine powered aircraft with clean and distorted inlet flows by Williams, J. G. (Author of Estimating engine airflow in gas-turbine powered aircraft with clean and distorted inlet flows)

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


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  16. 16
    Experimental investigation of unsteady shock wave turbulent boundary layer interactions about a blunt fin

    Experimental investigation of unsteady shock wave turbulent boundary layer interactions about a blunt fin by Barnhart, Paul J.

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


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  17. 17
    Design and predictions for a high-altitude (low-Reynolds-number) aerodynamic flight experiment

    Design and predictions for a high-altitude (low-Reynolds-number) aerodynamic flight experiment

    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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