Research Catalog

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  • Steady and unsteady three-dimensional transonic flow computations by integral equation method [microform] : final technical report / by Hong Hu, principal investigator.

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

  • Damage tolerant composite wing panels for transport aircraft [microform] / Peter J. Smith and Robert D. Wilson.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : National Technical Information Service, distributor], 1995.
    • 1985

  • Titanium honeycomb panel testing [microform] / W. Lance Richards, Randolph C. Thompson.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1996.
    • 1996

  • Thermostructural analysis of unconventional wing structures of a Hyper-X hypersonic flight research vehicle for the Mach 7 mission [microform] / William L. Ko and Leslie Gong.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS26693

  • Failure mechanisms of laminates transversely loaded by bolt push-through [microform] / William Allen Waters, Jr. and Jerry G. Williams.

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

    Available Online

    http://purl.access.gpo.gov/gPO/LPS85281

  • Composite transport wing technology development [microform] / Ram C. Madan.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1988]
    • 1988
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS89432

  • Fuel containment, lightning protection, and damage tolerance in large composite primary aircraft structures [microform] / Charles F. Griffin and Arthur M. James.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
    • 1985

  • Thermostructural evaluation of joggle region on the shuttle orbiter's wing leading edge / Sandra P. Walker and Jerry E. Warren.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo28056

  • Titanium honeycomb panel testing / W. Lance Richards, Randolph C. Thompson.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, October 1996.
    • 1996-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65662

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