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  • Innovative design of composite structures [microform] : design, manufacturing, and testing of plates utilitzing [sic] curvilinear fiber trajectories : final report for NASA / M.W. Hyer, R.J. Rust, W.A. Waters, Jr. ; prepared for M.P. Nemeth, Structural Mechanics Branch, NASA Langley Research Center.

    • Text
    • Blacksburg, VA : College of Engineering, Virginia Polytechnic Institute and State University ; Hampton, VA : Structural Mechanics Branch, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Serive, distributor, 1994]
    • 1994

  • Task 4 supporting technology [microform] / P.A. Hogenson, principal investigator.

    • Text
    • [Downey, Calif.] : Rockwell Aerospace, Space Systems Division ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Elevated temperature creep properties of NiAl cryomilled with and without Y₂O₃ [microform] / J. Daniel Whittenberger, Michael J. Luton.

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

  • A comparison of tension and compression creep in a polymeric composite and the effects of physical aging on creep [microform] / Thomas S. Gates, David R. Veazie, L. Catherine Brinson.

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

  • Test and analysis of composite hat stringer pull-off test specimens [microform] / Jian Li, T. Kevin O'Brien, Carl Q. Rousseau.

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

  • Effects of compression, staging, and braid angle on braided rope seal performance [microform] / Bruce M. Steinetz and Michael L. Adams.

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

  • Property evaluation of LTM25 composite materials [microform] / A.S. Postyn and C.H. Shah.

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

  • Experimental characterization and micromechanical modeling of woven carbon/copper composites [microform] / Brett A. Bednarcyk, Christopher C. Pauly, and Marek-Jerzy Pindera.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Standard test methods for textile composites [microform] / John E. Masters and Marc A. Portanova.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Isothermal fatigue, damage accumulation, and life prediction of a woven PMC [microform] / Andrew L. Gyekenyesi.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Investigations of control surface seals for re-entry vehicles [microform] / Patrick H. Dunlap ... [et al.] ; [prepared for the 38th Joint Propulsion Conference and Exhibit cosponsored by the AIAA, ASME, SAE, and ASEE, Indianapolis, Indiana, July 7-10, 2002].

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2002]
    • 2002

  • Investigations of control surface seals for re-entry vehicles [microform] / Dunlap, Patrick H. ; [prepared for 39th Joint Propulsion Conference and Exhibit ; cosponsored by the AIAA, ASME, SAE, and ASEE, Indianapolis, Indiana, July 7-10, 2002].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information, [2002]
    • 2002
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS36329

  • Compression failure mechanisms of composite structures [microform] / H. Thomas Hahn, Mohsen Sohi, and Suresh Moon.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
    • 1986

  • 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

  • Failure criterion of glass fabric reinforced plastic laminates [microform] / Osamu Haga, Noriyuki Hayashi, and Kzauo Kasuya.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, [1986]
    • 1986
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS92720

  • Effect of creep in titanium alloy Ti6Al-4V at elevated temperature on aircraft design and flight test [microform] / Jerald M. Jenkins.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1984.
    • 1984
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS95608

  • Scaling effects in the static large defelction response of graphite-epoxy composite beams / Karen E. Jackson, Edwin L. Fasanella.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center : US Army Aviation Systems Command, Aviation R&T Activity, [1989]
    • 1989
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS108701

  • Scaling effects in the static large defelction [i.e. deflection] response of graphite-epoxy composite beams [microform] / Karen E. Jackson, Edwin L. Fasanella.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center : US Army Aviation Systems Command, Aviation R&T Activity, [1989]
    • 1989

  • Investigation of the mechanical performance of compliant thermal barriers / Jeffrey J. DeMange, Robert J. Bott, Patrick H. Dunlap.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24057

  • Evaluation of ceramic honeycomb core compression behavior at room temperature / R. Keith Bird, Thomas S. LaPointe.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, February 2013.
    • 2013-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo49856

  • Effects of compression, staging, and braid angle on braided rope seal performance / Bruce M. Steinetz and Michael L. Adams.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, July 1997.
    • 1997-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo73164

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