Research Catalog

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  • Langley 16-ft. Transonic Tunnel Pressure Sensitive Paint System [microform] / Danny R. Sprinkle ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information (CASI), [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS28737

  • 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

  • Deployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight : preliminary PSP results from test 581 in the 14- x 22-foot subsonic tunnel / Anthony Neal Watkins ... [and others].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo22695

  • Measuring global surface pressures on a circulation control concept using pressure sensitive paint / Anthony Neal Watkins ... [and others].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo30920

  • Applying pressure sensitive paint technology to rotor blades / A. Neal Watkins [and five others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, May 2014.
    • 2014-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo52366

  • Pressure- and temperature-sensitive paint at 0.3-m transonic cryogenic tunnel / A. Neal Watkins [and three others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, September 2015.
    • 2015-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo64042

  • Experimental verification of buffet calculation procedure using unsteady PSP / Jayanta Panda.

    • Text
    • Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, February 2016.
    • 2016-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo67582

  • Assessment of JVX proprotor performance data in hover and airplane-mode flight conditions / C.W. Acree, Jr.

    • Text
    • Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, February 2016.
    • 2016-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo68686

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