Research Catalog

  • Improved speed control system for an 87,000 hp wind tunnel drive [microform] / Edward A. Becks, Timothy J. Bencic, Philip Z. Blumenthal.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Use of pressure sensitive paint for diagnostics in turbomachinery flows with shocks [microform] / Jan Lepicovsky, Timothy J. Bencic.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information, [2001]
    • 2000
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS30338
  • Experimental study of boundary layer flow control using an array of ramp-shaped vortex generators / Stefanie M. Hirt, Khairul B.M.Q. Zaman, and Timothy J. Bencic.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo32070
  • Boundary layer flow control by an array of ramp-shaped vortex generators / K. B. M. Q. Zaman, S. M. Hirt, and T .J. Bencic.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo28429

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