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  • Energy efficient engine [microform] : combustor component performance program / by D.J. Dubiel.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Energy efficient engine [microform] : acoustic supporting technology report / by S.P. Lavin and P.Y. Ho.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • Energy efficient engine component development and integration program [microform] : seventh semiannual status report, 1 April 1981 - 31 September 1981.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1981]
    • 1981

  • Integrated application of active controls (IAAC) technology to an advanced subsonic transport project [microform] : test ACT system description / prepared for Langley Research Center under contract NAS1-15325.

    • Text
    • Hampton, Va. : National Aeronautics and Space Admininstration, Langley Research Center, [1983]
    • 1983

  • A flight test of laminar flow control leading-edge systems [microform] / M.C. Fischer, A.S. Wright, Jr., and R. D. Wagner.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1983]
    • 1983

  • Airframe technology for aircraft energy efficiency [microform] / Robert L. James, Jr. and Dal V. Maddalon.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
    • 1984

  • Transonic steady- and unsteady-pressure measurements on a high-aspect-ratio supercritical-wing model with oscillating control surfaces [microform] / Maynard C. Sandford, Rodney H. Ricketts, and F.W. Cazier, Jr.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980.
    • 1980

  • Subsonic and transonic pressure measurements on a high-aspect-ratio supercritical-wing model with oscillating control surfaces [microform] / Maynard C. Sandford, Rodney H. Ricketts, and Judith J. Watson.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, [1981]
    • 1981
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS97353

  • Steady- and unsteady-pressure measurements on a supercritical wing model with oscillating control surfaces at subsonic and transonic speeds [microform] / Maynard C. Sandford and Rodney H. Ricketts.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1983.
    • 1983

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