Research Catalog

New! Try our Article Search to discover online journals, books, and more from home with your library card.

Selected filters.Clear Filters

  • Aerodynamic characteristics of several current helicopter tail boom cross sections including the effect of spoilers [microform] / John C. Wilson and Henry L. Kelley.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service, distributor], 1986.
    • 1986

  • Reynolds number effects on the performance of lateral control devices [microform] / Raymond E. Mineck.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [2000]
    • 2000

  • Boeing/NASA composite components flight service evaluation [microform] / Randy L. Coggeshall.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67932

  • 737 graphite composite flight spoiler flight service evaluation [microform] : eighth report / Randy L. Coggeshall.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS88061

  • Flight measurements of hinged-plate wing-spoiler hinge moments [microform] / Emmett B. Fry.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1983]
    • 1983
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS99705

  • An experimental study of airfoil-spoiler aerodynamics [microform] / Blair G. McLachlan and K. Karamcheti.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1985]
    • 1985

  • Reynolds number effects on the performance of lateral control devices / Raymond E. Mineck.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, October 2000.
    • 2000-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo86203

No results found from Digital Research Books Beta

Digital books for research from multiple sources world wide- all free to read, download, and keep. No Library Card is Required. Read more about the project.

digital-research-book
Explore Digital Research Books Beta