Research Catalog

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  • A study of three dimensional turbulent boundary layer separation and vortex flow control using the reduced Navier Stokes equations [microform] / Bernhard H. Anderson and Saeed Farokhi.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
    • 1991

  • Application of computational fluid dynamics to the study of vortex flow control for the management of inlet distortion [microform] / Bernhard H. Anderson and James Gibb.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1992]
    • 1992

  • A design strategy for the use of vortex generators to manage inlet-engine distortion using computational fluid dynamics [microform] / Bernhard H. Anderson and Ralph Levy.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • The aerodynamic characteristics of vortex ingestion for the F/A-18 inlet duct [microform] / Bernhard H. Anderson.

    • Text
    • [Washington, DC] : NASA ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • A robust design methodology for optimal microscale secondary flow control in compact inlet diffusers [microform] / Bernhard H. Anderson, Dennis J. Keller.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS26473

  • Management of total pressure recovery, distortion and high cycle fatigue in compact air vehicle inlets [microform] / Bernhard H. Anderson, Henry D. Baust, Johan Agrell.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information, [2002]
    • 2002
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS36341

  • Design-of-experiments to reduce life-cycle costs in combat aircraft inlets [microform] / Bernhard H. Anderson, Henry D. Baust, [and] Johan Agrell.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information, [2003]
    • 2003
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS46082

  • Three-dimensional viscous design methedology for advanced technology aircraft supersonic inlet systems [microform] / Bernhard H. Anderson.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1984]
    • 1984

  • Management of total pressure recovery, distortion and high cycle fatigue in compact air vehicle inlets / Bernhard H. Anderson, Henry D. Baust, Johan Agrell.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 2002.
    • 2002-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS36341

  • Design-of-experiments to reduce life-cycle costs in combat aircraft inlets / Bernhard H. Anderson, Henry D. Baust, Johan Agrell.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, January 2003.
    • 2003-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS46082

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