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  • Forced response testing of an axi-centrifugal turboshaft engine [microform] / A. Karl Owen ... [et al.].

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, U.S. Army Research Laboratory ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Dimension determination of precursive stall events in a single stage high speed compressor [microform] / Michelle M. Bright, Helen K. Qammar and Tom T. Hartley.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Dynamic modeling of starting aerodynamics and stage matching in an axi-centrifugal compressor [microform] / Kevin Wilkes and Walter F. O'Brien, A. Karl Owen.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Comparisons of rig and engine dynamic events in the compressor of an axi-centrifugal turboshaft engine [microform] / A. Karl Owen, Duane L. Mattern, Dzu K. Le.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Self-recirculating casing treatment concept for enhanced compressor performance [microform] / Michael D. Hathaway ; [prepared for the Turbo Expo 2002 ; cosponsored by the American Society of Mechanical Engineers and the International Gas Turbine Institute, Amsterdam, the Netherlands, June 3-6, 2002].

    • 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/LPS36325

  • Flow mechanism and experimental investigation of a rotating stall in transonic compressors [microform] / Lu Yajun and Zhang Shunlin.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, [1983]
    • 1983

  • Dimension determination of precursive stall events in a single stage high speed compressor / Michelle M. Bright, Helen K. Qammar and Tom T. Hartley.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, July 1996.
    • 1996-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo69462

  • Dynamic modeling of starting aerodynamics and stage matching in an axi-centrifugal compressor / Kevin Wilkes and Walter F. O'Brien, A. Karl Owen.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center : U.S. Army Research Laboratory, October 1996.
    • 1996-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo70387

  • Comparisons of rig and engine dynamic events in the compressor of an axi-centrifugal turboshaft engine / A. Karl Owen, Duane L. Mattern, Dzu K. Le.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center : U.S. Army Research Laboratory, October 1996.
    • 1996-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo70389

  • On hammershock propagation in a supersonic flow field / A. Robert Porro.

    • Text
    • Cleveland Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2002.
    • 2002-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS68703

  • An investigation of surge in a high-speed centrifugal compressor using digital PIV / Mark P. Wernet and Michelle M. Bright, Gary J. Skoch.

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

    Available Online

    https://purl.fdlp.gov/GPO/LPS43729

  • Methods for computationally efficient structured CFD simulations of complex turbomachinery flows / Gregory P. Herrick, Jen-Ping Chen.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo29068

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