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  • Aeroelastic simulation of higher harmonic control [microform] / Lawson H. Robinson and Peretz P. Friedmann.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Higher harmonic control analysis for vibration reduction of helicopter rotor systems [microform] / Khanh O. Nguyen.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Toward comparing experiment and theory for corroborative research on hingeless rotor stability in forward flight [microform] : final technical report under NASA-Ames cooperative agreement no. NCC 2-361 (August 1, 1985 - July 31, 1987) / by G. Gaonkar.

    • Text
    • Boca Raton, FL : Florida Atlantic University, Dept. of Mechanical Engineering, School of Engineering ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • Application of higher harmonic control to hingeless rotor systems [microform] / Khanh Nguyen and Inderjit Chopra.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
    • 1991

  • Full-scale hingeless rotor performance and loads [microform] / Randall L. Peterson.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Aeroelastic stability of a full-scale hingeless rotor [microform] / Randall L. Peterson and Khanh Nguyen.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • The effects of structural flap-lag and pitch-lag coupling on soft inplane hingeless rotor stability in hover [microform] / William G. Bousman.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1990.
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS65436

  • Hover test of a full-scale hingeless helicopter rotor [microform] : aeroelastic stability, performance, and loads data / William Warmbrodt, Randall L. Peterson.

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

  • 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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