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  • A comparison of graphite/epoxy tape laminates and 2-D braided composites mechanical properties [microform] / Pierre J. Minguet and Christian K. Gunther.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Test methods for textile composites [microform] / Pierre J. Minguet, Mark J. Fedro, and Christian K. Gunther.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Novel matrix resins for composites for aircraft primary structure [microform] / E.P. Woo ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • Combined compressive and shear buckling analysis of hypersonic aircraft structural sandwich panels [microform] / William L. Ko and Raymond H. Jackson.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor], 1991.
    • 1991

  • Reliability-based failure analysis of brittle materials [microform] / Lynn M. Powers and Louis J. Ghosn.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Compression strength of composite primary structural components [microform] : semiannual status report : performance period: May 1, 1994 to October 31, 1994 / Eric R. Johnson, principal investigator.

    • Text
    • Blacksburg, Va. : Aerospace and Ocean Engineering Dept., Virginia Polytechnic and State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1994

  • Experimental observations and finite element analysis of the initiation of fiber microbuckling in notched composite laminates [microform] : an annual progress report / prepared by E. Gail Guynn, Walter L. Bradley.

    • Text
    • College Station, Tex. : Center for Mechanics of Composites, Texas A&M University ; [Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1989

  • Effects of through-the-thickness stitching on impact and interlaminar fracture properties of textile graphite/epoxy laminates [microform] / Suresh K. Sharma and Bhavani V. Sankar.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Microstructure and properties of cryomilled nickel aluminide extruded with chromium or molybdenum [microform] / Beverly J.M. Aikin, Robert M. Dickerson, and Patricia O. Dickerson.

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

  • The effects of compressive preloads on the compression-after-impact strength of carbon/epoxy [microform] / Alan T. Nettles.

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

  • A thermostructural analysis of a diboride composite leading edge [microform] / Tom Kowalski ... [et al.].

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

  • Planetary and primitive object strength measurements and sampling apparatus [microform] : NASA #NAGW 2439, final report; February 1, 1991 through January 31, 1997 / Thomas J. Ahrens, principal investigator.

    • Text
    • Pasadena, Calif. : California Institute of Technology, Seismological Laboratory ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • 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

  • Thermal and mechanical durability of graphite-fiber-reinforced PMR-15 composites [microform] / K.J. Bowles.

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

  • Elevated temperature compressive strength properties of oxide dispersion strengthened NiAl after cryomilling and roasting in nitrogen [microform] / J. Daniel Whittenberger ... [et al.].

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

  • Low cost manufacturing approach of high temperature PMC components [microform] / Kevin Kannmacher.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, VA : National Technical Information Service, distributor, [1997]
    • 1997

  • 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

  • Evaluation of the transient liquid phase (TLP) bonding process for Ti₃-Based honeycomb core sandwich structure [microform] / R. Keith Bird and Eric K. Hoffman.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998

  • Thermal/mechanical response of a polymer matrix composite at cryogenic temperatures [microform] / Karen S. Whitley and Thomas S. Gates.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2003]
    • 2003
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS55059

  • 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

  • Mechanical strength and thermophysical properties of PM212 [microform] : a high temperature self-lubricating powder metallurgy composite / Phillip M. Edwards, ... [et al.].

    • Text
    • [Cleveland, Ohio : Lewis Research Center, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS64162

  • Concepts for improving the damage tolerance of composite compression panels [microform] / Marvin D. Rhodes, Jerry G. Williams.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS95389

  • Effect of impact damage and open holes on the compression strength of tough resin/high strain fiber laminates [microform] / Jerry G. Williams.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS95394

  • A damage tolerance comparison of composite hat-stiffened and honeycomb sandwich structure for launch vehicle interstage applications / A.T. Nettles.

    • Text
    • Huntsville, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24323

  • Notched strength allowables and inplane shear strength of AS4/VRM-34 textile laminates / Ray W. Grenoble, William M. Johnston.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, October 2013.
    • 2013-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo50482

  • Evaluation of the behavior of Technova Corporation rod-stiffened stitched compression specimens / Dawn C. Jegley.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo50839

  • Elevated temperature compressive strength properties of oxide dispersion strengthened NiAl after cryomilling and roasting in nitrogen / J. Daniel Whittenberger [and others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, July 1998.
    • 1998-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo83113

  • The effect of impact damage next to holes on the bearing strength of carbon fiber laminates / A.T. Nettles.

    • Text
    • Huntsville, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, December 2019.
    • 2019-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo130586

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