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  1. 1
    Active control of instabilities in laminar boundary-layer flow

    Active control of instabilities in laminar boundary-layer flow by Joslin, Ronald D. (Ronald Douglas), 1963-

    Hampton, VA : [Springfield, Va.] : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [National Technical Information Service, distributor], 1994
    Format: Government Document Book


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  2. 2
    Experiments to verify nonparallel stability theory at Virginia Polytechnic Institute and State University, Blacksburg, Virginia : final report

    Experiments to verify nonparallel stability theory at Virginia Polytechnic Institute and State University, Blacksburg, Virginia : final report by Saric, W. S.

    Tempe, Ariz. : [Washington, DC] : [Springfield, Va.] : Dept. of Mechanical and Aerospace Engineering, Arizona State University ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1988
    Format: Government Document Book


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  3. 3
    High Reynolds number hybrid laminar flow control (HLFC) flight experiment. II, Aerodynamic design

    High Reynolds number hybrid laminar flow control (HLFC) flight experiment. II, Aerodynamic design

    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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  4. 4
    Vortex/boundary-layer interactions, data report final report on NASA grant NAGw-581

    Vortex/boundary-layer interactions, data report final report on NASA grant NAGw-581 by Cutler, A. D.

    London : [Springfield, Va. : Imperial College of Science and Technology, Dept. of Technology ; For sale by the National Technical Information Service, 1987
    Format: Government Document Book


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  5. 5
    Active control of boundary-layer instabilities : use of sensors and spectral controller

    Active control of boundary-layer instabilities : use of sensors and spectral controller

    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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  6. 6
    Boundary layer and flow control : its principles and application.

    Boundary layer and flow control : its principles and application.

    New York : Pergamon Press, 1961
    Format: Book


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  7. 7
    F-16XL-2 supersonic laminar flow control flight test experiment

    F-16XL-2 supersonic laminar flow control flight test experiment by Anders, Scott G.

    Hampton, Va. : Hanover, Md. : Springfield, Va. : National Aeronautics and Space Administration, Langley Research Center ; Available from NASA Center for AeroSpace Information ; National Technical Information Service [distributor], 1999
    Format: Government Document Book


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  8. 8
    Approximation of discrete-time LQG compensators for distributed systems with boundary input and unbounded measurement

    Approximation of discrete-time LQG compensators for distributed systems with boundary input and unbounded measurement by Gibson, J. S. (John Sevier), 1934-

    Hampton, Va. : [Springfield, Va.] : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [For sale by the National Technical Information Service], 1987
    Format: Government Document Book


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  9. 9
    Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment

    Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment by Marshall, Laurie A.

    Edwards, Calif. : Hanover, Md. : Springfield, Va. : National Aeronautics and Space Administration, Dryden Flight Research Center ; NASA Center for AeroSpace Information [distributor] ; National Technical Information Service [distributor], 1999
    Format: Government Document Book


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  10. 10
    Effect of nonzero surface admittance on receptivity and stability of compressible boundary layer

    Effect of nonzero surface admittance on receptivity and stability of compressible boundary layer by Choudhari, Meelan

    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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  11. 11
    Flow characteristics in boundary layer bleed slots with plenum

    Flow characteristics in boundary layer bleed slots with plenum by Hamed, A. (Awatef)

    [Washington, D.C.] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [For sale by the National Technical Information Service], 1995
    Format: Government Document Book


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  12. 12
    Semi-annual status report on research grant no. NAGW-581 Vortex boundary-layer interactions, period 1 March 1986 - 31 August 1986.

    Semi-annual status report on research grant no. NAGW-581 Vortex boundary-layer interactions, period 1 March 1986 - 31 August 1986.

    London : Imperial College of Science and Technology, Dept. of Aeronautics, 1986
    Format: Government Document Book


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  13. 13
    Analysis of the leading edge effects on the boundary layer transition : technical report, March 1, 1984 - August 31, 1990

    Analysis of the leading edge effects on the boundary layer transition : technical report, March 1, 1984 - August 31, 1990 by Chow, P. L. (Pao Liu), 1936-

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


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  14. 14
    Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction final report

    Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction final report by Nagamatsu, H. T.

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


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  15. 15
    Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction : final report on NASA grant NAG 1-1471 for the period 01/09/93 through 01/01/95

    Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction : final report on NASA grant NAG 1-1471 for the period 01/09/93 through... by Dolling, David S.

    Austin, Tex. : [Washington, DC] : [Springfield, Va.] : Center for Aerodynamics Research, Dept. of Aerospace Engineering & Engineering Mechanics, University of Texas at Austin ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  16. 16
    Boundary layer flow control with a One Atmosphere Uniform Glow Discharge Surface Plasma

    Boundary layer flow control with a One Atmosphere Uniform Glow Discharge Surface Plasma by Roth, J. Reece

    Reston, Va. : [Washington, DC] : [Springfield, Va.] : American Institute of Aeronautics and Astronautics ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1998
    Format: Government Document Book


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  17. 17
    Supersonic laminar flow control research : semiannual report #4, July 1995 - December 1995

    Supersonic laminar flow control research : semiannual report #4, July 1995 - December 1995 by Lo, C. F.

    Moffett Field, Calif. : [Springfield, Va.] : Ames Research Center ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  18. 18
    Physics of forced unsteady separation proceedings of a NASA/AFOSR/ARO workshop held at NASA Ames Research Center, Moffett Field, California, April 17-19, 1990

    Physics of forced unsteady separation proceedings of a NASA/AFOSR/ARO workshop held at NASA Ames Research Center, Moffett Field, California, April 17-19, 1990

    Moffett Field, Calif. : Ames Research Center, 1992
    Format: Government Document Book


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  19. 19
    High Reynolds number hybrid laminar flow control (HLFC) flight experiment. IV, Suction system design and manufacture

    High Reynolds number hybrid laminar flow control (HLFC) flight experiment. IV, Suction system design and manufacture

    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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  20. 20
    Closed-loop separation control using oscillatory flow excitation

    Closed-loop separation control using oscillatory flow excitation

    Hampton, Va. : Hanover, MD : ICASE, National Aeronautics and Science Administration, Langley Research Center ; Available from NASA Center for Aerospace Information, 2000
    Format: Government Document Book


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