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  • 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

  • Final technical report on grant NAG3-1567 entitled Inlet distortion in engines on VSTOL aircraft [microform] / submitted to NASA Lewis Research Center ; principal investigator Choon S. Tan, co-investigator Edward M. Greitzer.

    • Text
    • Cleveland, OH : The Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application [microform] / Kamlesh Kapoor, Bernard H. Anderson, and Robert J. Shaw.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Summary of investigations of engine response to distorted inlet conditions [microform] / Thomas J. Biesiadny ... [et al.].

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1986?]
    • 1986

  • PARC3D calculations of the F/A-18A HARV inlet vortex generators [microform] / Steve D. Podleski.

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

  • Dynamic inlet distortion prediction with a combined computational fluid dynamics and distortion synthesis approach [microform] / W.P. Norby, J.A. Ladd, and A.J. Yuhas.

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

  • Linear instability of a uni-directional transversely sheared mean flow [microform] / David W. Wundrow.

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

  • High stability engine control (HISTEC) [microform] / John C. DeLaat, Robert D. Southwick and George W. Gallops.

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

  • Estimating engine airflow in gas-turbine powered aircraft with clean and distorted inlet flows [microform] / J.G. Williams and W.G. Steenken, A.J. Yuhas.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate) [microform] : under cooperative agreement NCC1-241 / M.N. Kogan and M.V. Ustinov.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • High stability engine control (HISTEC) flight test results [microform] / Robert D. Southwick ... [et al.].

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

  • Nonlinear interaction of detuned instability waves in boundary-layer transition [microform] : amplitude equations / Sang Soo Lee.

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

  • High stability engine control (HISTEC) [microform] : flight demonstration results / John C. DeLaat ... [et al.].

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

  • The high stability engine control (HISTEC) program [microform] : flight demonstration phase / John C. DeLaat ... [et al.].

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

  • Theoretical and experimental study of flow-control devices for inlets of indraft wind tunnels [microform] / James C. Ross.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67453

  • High stability engine control (HISTEC) / John C. DeLaat, Robert D. Southwick and George W. Gallops.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, June 1996.
    • 1996-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo69482

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