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  • Wake geometry measurements and analytical calculations on a small-scale rotor model [microform] / Terence A. Ghee ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Computation of helicopter rotor acoustics in forward flight [microform] / Roger Strawn, Rupak Biswas.

    • Text
    • [Moffett Field, Calif.] : Research Institute for Advanced Computer Science, NASA Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Numerical simulation of helicopter engine plume in forward flight [microform] : final report cooperative agreement #NCC2-5061 / Arsenio C.B. Dimanlig, Cornelis P. van Dam, Earl P.N. Duque.

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

  • Convective heat transfer from castings of ice roughened surfaces in horizontal flight [microform] / Nihad Dukhan ... [et al.].

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

  • XV-15 structural-acoustic data [microform] / Karen H. Lyle.

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

  • Final report for ETP-0403, Residual stress measurements after proof and flight [microform].

    • Text
    • Brigham City, UT : Thiokol ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Unsteady velocity measurements taken behind a model helicopter rotor hub in forward flight [microform] / John D. Berry.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1997]
    • 1997
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60757

  • V/STOL maneuverability and control [microform] / James A. Franklin and Seth B. Anderson.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1984]
    • 1984

  • 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

  • Application of a high-fidelity icing analysis method to a model-scale rotor in forward flight / Robert Narducci and Stanley Orr, Richard E. Kreeger.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo24995

  • Aeroacoustic experiments with twin jets / Richard F. Bozak and Brenda S. Henderson.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo28440

  • 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

  • Aeromechanical stability of a hingeless rotor in hover and forward flight : analysis and wind tunnel tests / William T. Yeager, Jr., M-Nabil H. Hamouda, Wayne R. Mantay.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 1983.
    • 1983-8

  • Aeromechanical stability of a hingeless rotor in hover and forward flight : analysis and wind tunnel tests / William T. Yeager, Jr., M-Nabil H. Hamouda, Wayne R. Mantay.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 1983.
    • 1983-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo62349

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