Showing 1 - 17 results of 17 for search 'Anderson, Bernhard H.', query time: 0.06s Refine Results
  1. 1
    A design strategy for the use of vortex generators to manage inlet-engine distortion using computational fluid dynamics

    A design strategy for the use of vortex generators to manage inlet-engine distortion using computational fluid dynamics by Anderson, Bernhard H.

    [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
    Management of total pressure recovery, distortion and high cycle fatigue in compact air vehicle inlets

    Management of total pressure recovery, distortion and high cycle fatigue in compact air vehicle inlets by Anderson, Bernhard H.

    Cleveland, Ohio : Hanover Md. :; Cleveland, Ohio : Hanover MD : National Aeronautics and Space Administration, Glenn Research Center ; Available from NASA Center for AeroSpace Information, 2002
    Format: Government Document Book


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  3. 3
    The aerodynamic characteristics of vortex ingestion for the F/A-18 inlet duct

    The aerodynamic characteristics of vortex ingestion for the F/A-18 inlet duct by Anderson, Bernhard H.

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


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  4. 4
    A study of three dimensional turbulent boundary layer separation and vortex flow control using the reduced Navier Stokes equations

    A study of three dimensional turbulent boundary layer separation and vortex flow control using the reduced Navier Stokes equations by Anderson, Bernhard H.

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


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  5. 5
    A study of three dimensional turbulent boundary layer separation and vortex flow control using the reduced Navier Stokes equations

    A study of three dimensional turbulent boundary layer separation and vortex flow control using the reduced Navier Stokes equations by Anderson, Bernhard H.

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


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  6. 6
    A design strategy for the use of vortex generators to manage inlet-engine distortion using computational fluid dynamics

    A design strategy for the use of vortex generators to manage inlet-engine distortion using computational fluid dynamics by Anderson, Bernhard H.

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


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  7. 7
    Application of computational fluid dynamics to the study of vortex flow control for the management of inlet distortion

    Application of computational fluid dynamics to the study of vortex flow control for the management of inlet distortion by Anderson, Bernhard H.

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [For sale by the National Technical Information Service], 1992
    Format: Government Document Book


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  8. 8
    A robust design methodology for optimal microscale secondary flow control in compact inlet diffusers

    A robust design methodology for optimal microscale secondary flow control in compact inlet diffusers by Anderson, Bernhard H.

    [Cleveland, Ohio] : Hanover, Md. :; [Cleveland, Ohio] : Hanover, MD : National Aeronautics and Space Administration, Glenn Research Center ; Available from NASA Center for Aerospace Information, 2001
    Format: Government Document Book


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  9. 9
    The aerodynamic characteristics of vortex ingestion for the F/A-18 inlet duct

    The aerodynamic characteristics of vortex ingestion for the F/A-18 inlet duct by Anderson, Bernhard H.

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


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  10. 10
    Design-of-experiments to reduce life-cycle costs in combat aircraft inlets

    Design-of-experiments to reduce life-cycle costs in combat aircraft inlets by Anderson, Bernhard H.

    [Cleveland, Ohio] : Hanover Md. :; Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center ; Available from NASA Center for AeroSpace Information,; National Aeronautics and Space Administration, Glenn Research Center, 2003
    Format: Government Document Book


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  11. 11
    A study on vortex flow control on inlet distortion in the re-engined 727-100 center inlet duct using computational fluid dynamics

    A study on vortex flow control on inlet distortion in the re-engined 727-100 center inlet duct using computational fluid dynamics

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1992
    Other Authors: “…Anderson, Bernhard H.…”
    Format: Government Document Book


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  12. 12
    Internal fluid mechanics research on supercomputers for aerospace propulsion systems

    Internal fluid mechanics research on supercomputers for aerospace propulsion systems by Miller, Brent A.

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1988
    Other Authors: “…Anderson, Bernhard H.…”
    Format: Government Document Book


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  13. 13
    Internal fluid mechanics research on supercomputers for aerospace propulsion systems

    Internal fluid mechanics research on supercomputers for aerospace propulsion systems by Miller, Brent A.

    [Washington, DC : Springfield, Va. : National Aeronautics and Space Administration ; National Technical Information Service, distributor, 1988
    Other Authors: “…Anderson, Bernhard H.…”
    Format: Government Document Book


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  14. 14
    Wall and bottom heating of liquid hydrogen in a propellant tank

    Wall and bottom heating of liquid hydrogen in a propellant tank by Huntley, Sidney C.

    Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1966
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    Format: Government Document Book


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  15. 15
    Comparative study of turbulence models in predicting hypersonic inlet flows

    Comparative study of turbulence models in predicting hypersonic inlet flows by Kapoor, Kamlesh

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1992
    Other Authors: “…Anderson, Bernhard H.…”
    Format: Government Document Book


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  16. 16
    A full Navier-Stokes analysis of subsonic diffuser of a bifurcated 70/30 supersonic inlet for high speed civil transport application

    A full Navier-Stokes analysis of subsonic diffuser of a bifurcated 70/30 supersonic inlet for high speed civil transport application by Kapoor, Kamlesh

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1994
    Other Authors: “…Anderson, Bernhard H.…”
    Format: Government Document Book


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  17. 17
    Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code

    Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code by Kapoor, Kamlesh

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1994
    Other Authors: “…Anderson, Bernhard H.…”
    Format: Government Document Book


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