Research Catalog

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  • Numerical simulation of Gortler/Tollmien-Schlichting wave-interaction [microform] / M.R. Malik, M.Y. Hussaini.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Grid resolution and turbulent inflow boundary condition recommendations for NPARC calculations [microform] / Nicholas J. Georgiadis and Julianne C. Dudek and Thomas P. Tierney.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream [microform] / George C. Olsen and Robert J. Nowak.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • An investigation of bleed configurations and their effect on shock wave/boundary layer interactions [microform] : final report / Awatef Hamed, principal investigator.

    • Text
    • [Cincinnati, Ohio?] : University of Cincinnati ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Numerical simulation of supersonic flow using a new analytical bleed boundary condition [microform] / G.J. Harloff and G.E. Smith.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Flow characteristics in boundary layer bleed slots with plenum [microform] / A. Hamed, J.J. Yeuan and J.D. Jun.

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

  • Screech tones from rectangular jets with spanwise oblique shock-cell structures [microform] : [final contractor report] / Ganesh Raman.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, [Lewis Research Center ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Computation of thermally perfect properties of oblique shock waves [microform] : under contract NAS1-19000 / Kenneth E. Tatum.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction [microform] / D.O. Davis, B.P. Willis, and W.R. Hingst.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998

  • Effects of convoluted divergent flap contouring on the performance of a fixed-geometry nonaxisymmetric exhaust nozzle [microform] / Scott C. Asbury and Craig A. Hunter.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • Mach 10 experimental database of a three-dimensional scramjet inlet flow field [microform] / Scott D. Holland.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, VA : Available from the National Technical Information Service, 1995]
    • 1995
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60779

  • Interactive calculation procedures for mixed compression inlets [microform] / Eli Reshotko.

    • Text
    • Cleveland, Ohio : Dept. of Mechanical and Aerospace Engineering, School of Engineering, Case Institute of Technology, Case Western Reserve University, [1983]
    • 1983
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60916

  • Flow separation in shock wave boundary layer interactions at hypersonic speeds [microform] / A. Hamed.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS61576

  • Micro-ramp flow control for oblique shock interactions : comparisons of computational and experimental data / Stefanie M. Hirt, David B. Reich, Michael B. O'Connor.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo30949

  • Wind-US code contributions to the first AIAA Shock Boundary Layer Interaction Prediction Workshop / Nicholas J. Georgiadis, Manan A. Vyas, and Dennis A. Yoder.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2013.
    • 2013
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo51482

  • Shock generation and control using DBD plasma actuators : SBIR phase I final report / by Mehul P. Patel [and four others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo32876

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