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  • Inlet flow characteristics during rapid maneuvers for an F/A-18A airplane [microform] / William G. Steenken and John G. Williams, Kevin R. Walsh.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • Three dimensional viscous analysis of a hypersonic inlet [microform] / D.R. Reddy ... [et al.].

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1989?]
    • 1989

  • Prediction of wind tunnel effects on the installed F/A-18A inlet flow field at high angles-of-attack [microform] / Crawford F. Smith.

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

  • Flow in out-of-plane double s-bends [microform] / by M.C. Schmidt, J.H. Whitelaw and M. Yianneskis.

    • Text
    • London, England : Imperial College of Science and Technology, Fluids Section, Mechanical Enginering Dept. : [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Hydrodynamic design of the fastrac turbopump [microform] / Roberto Garcia and Robert Williams, Shawn Fears.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Propulsion flight research at NASA Dryden from 1967 to 1997 [microform] / Frank W. Burcham, Jr. ... [et al.].

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Unsteady ejector performance [microform] : an experimental investigation using a pulsejet driver / Daniel E. Paxson, Jack Wilson and Kevin T. Dougherty.

    • 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/LPS30958

  • The structural dynamics analysis of the main injector LOX inlet tee and its redesign [microform] / [E. Romano].

    • Text
    • [Canoga Park, Calif. : Rockwell International, Rocketdyne Division? ; Washington, D.C. : National Aeronautics and Space Administration?, 1989?]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69840

  • Analytical study of blowing boundary-layer control for subsonic V/STOL inlets [microform] / Danny P. Hwang.

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

  • Evaluation of capillary reinforced composites / by Samuel W. Ciardullo and Lewis J. Stoffer.

    • Text
    • Cincinnati, Ohio : General Electric Company, Aircraft Engine Business Group ; [Cleveland, Ohio] : National Aeronautics and Space Administration, NASA Lewis Research Center, [1985]
    • 1985
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24654

  • Multiphysics modeling of an annular linear induction pump with applications to space nuclear power systems / J. Kilbane and K.A. Polzin.

    • Text
    • Huntsville, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, March 2014.
    • 2014-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo51424

  • Analysis of flow dynamics through small diameter gas sampling systems / by Kenneth G. Brown, principal investigator.

    • Text
    • Norfolk, Virginia : Old Dominion University Research Foundation ; Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, February 1984.
    • 1984-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo48072

  • Analysis of flow dynamics through small diameter gas sampling systems / by Kenneth G. Brown, principal investigator.

    • Text
    • Norfolk, Virginia : Old Dominion University Research Foundation ; Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, February 1984.
    • 1984-2

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