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  • Mechanical response of thick laminated beams and plates subject to out-of-plane loading [microform] / C.C. Hiel, H.F. Brinson.

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

  • Atomic oxygen durability evaluation of the flexible batten for the photovoltaic array mast on Space Station [microform] / Curtis R. Stidham ... [et al.].

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

  • Post-impact fatigue of cross-plied, through-the-thickness reinforced carbon/expoxy composites [microform] / by Thomas E. Serdinak.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1994

  • Composite processing development to improve interlaminar strength using ply interface particles [microform] : (Center Director's discretionary fund final report, no. 93-13) / A.T. Nettles.

    • Text
    • MSFC, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Strain energy release rate analysis of delamination in a tapered laminate subjected to tension load [microform] / S.A. Salpekar, I.S. Raju, and T.K. O'Brien.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center : US Army Aviation Systems Command, Aviation R&T Activity ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • The effects of tensile preloads on the impact response of carbon/epoxy laminates [microform] / Alan Nettles, Vince Daniel, Caleb Branscomb.

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

  • Impact damage resistance of carbon/epoxy composite tubes for the DC-XA liquid hydrogen feedline [microform] / A.T. Nettles.

    • Text
    • MSFS, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Failure models for textile composites [microform] / Brian Cox.

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

  • An acoustic emission and acousto-ultrasonic analysis of impact damaged composite pressure vessels [microform] / prepared by James L. Walker ; principal investigator, Gary L. Workman.

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

  • Properties of two carbon composite materials using LTM25 epoxy resin [microform] / Juan R. Cruz, C.H. Shah, and A.S. Postyn.

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

  • Design and evaluation of a bolted joint for a discrete carbon-epoxy rod-reinforced hat section [microform] / Donald J. Baker, Carl Q. Rousseau.

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

  • 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

  • Analysis of thick sandwich shells with embedded ceramic tiles [microform] / Carlos G. Davila, C. Smith and F. Lumban-Tobing.

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

  • Prediction of composite laminate fracture [microform] : micromechanics and progressive fracture / P.K. Gotsis and C.C. Chamis, L. Minnetyan.

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

  • The charging of composites in the space environment [microform] / by Steven A. Czepiela.

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

  • A progressive damage methodology for residual strength predictions of notched composite panels [microform] / Timothy W. Coats and Charles E. Harris.

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

  • Rapid prototyping of composite structures [microform] : annual performance report, performance period 7/14/97 to 6/30/98 : NASA LaRC #NLPN 97-620, GT # E25-A55 / PI, Jonathan S. Colton.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • The impact response of carbon/epoxy laminates [microform] / A.T. Nettles and A.J. Hodge.

    • Text
    • [Huntsville, Ala.] : National Aeronautics and Space Administration, Marshall Space Flight Center ; Springfield, VA : National Technical Information Service, distributor, [1997]
    • 1997

  • Scaling effects in carbon/epoxy laminates under transverse quasi-staic loading [microform] / Alan T. Nettles, Michael J. Douglas, Eric E. Estes.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • Fatigue life methodology for tapered composite flexbeam laminates [microform] / Gretchen B. Murri, T. Kevin O'Brien, Carl Q. Rousseau.

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

  • An experimental study of a stitched composite with a notch subjected to combined bending and tension loading [microform] / Susan O. Palmer, Alan T. Nettles, and C.C. Poe, Jr.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • Impact testing of composites for aircraft engine fan cases [microform] / Gary D. Roberts ... [et al.].

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS26848

  • Fracture behavior of a stitched warp-knit carbon fabric composite [microform] / Clarence C. Poe, James R. Reeder, F.G. Yuan.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS27205

  • Influence of specimen preparation and specimen size on composite transverse tensile strength and scatter [microform] / T. Kevin O'Brien ... [et al.].

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS27427

  • Transverse tension fatigue life characterization through flexure testing of composite materials [microform] / T. Kevin O'Brien ... [et al.].

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS27494

  • Open hole and post-impact compression fatigue of stitched and unstitched carbon/epoxy composites [microform] / M.A. Portanova, C.C. Poe, Jr., and John D. Whitcomb.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS58754

  • Resistivity of pristine and intercalated graphite fiber epoxy composites [microform] / James R. Gaier, Paul D. Hambourger, and Melissa E. Slabe ; prepared for the 19th Biennial Conference on Carbon sponsored by the American Carbon Society, University Park, Pennsylvania, June 25-30, 1989.

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS66859

  • Cross-sectional examination of the damage zone in impacted specimens of carbon/epoxy and carbon/peek composites [microform] / by A.T. Nettles and N.J. Magold.

    • Text
    • [Marshall Space Flight Center, Ala.] : National Aeronautics and Space Administration, George C. Marshall Space Flight Center ; [Springfield, VA : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67327

  • Instrumented impact and residual tensile strength testing of eight-ply carbon/epoxy specimens [microform] / A.T. Nettles.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, VA : For sale by the National Technical Information Service], 1990.
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS68606

  • Properties of carbon fibers with various coatings [microform] / Volker Seegel and Paul McMahon.

    • Text
    • Washington, DC : National Aeronautics and Space Administration, [1983]
    • 1983

  • Effects of seawater and deionized water at 0⁰ to 80⁰C on the flexural properties of a glass/epoxy composite [microform] / B. G. Penn ... [et al.].

    • Text
    • [Marshall Space Flight Center, Ala.] : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1986]
    • 1986

  • 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

  • Buckling testing and analysis of honeycomb sandwich panel arc segments of a full-scale fairing barrel / David E. Myers, Evan J. Pineda [and four others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2013-2014.
    • 2013-2014
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo51535

  • Evaluation of nanomaterial approaches to damping in epoxy resin and carbon fiber/epoxy composite structures by dynamic mechanical analysis / Sandi G. Miller [and five others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2013.
    • 2013-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo51765

  • Composite materials with uncured epoxy matrix exposed in stratosphere during NASA stratospheric balloon flight / Alexey Kondyurin [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, May 2013.
    • 2013-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo40535

  • Analysis of fiber clustering in composite materials using high-fidelity multiscale micromechanics / Brett A. Bednarcyk, Jacob Aboudi, Steven M. Arnold.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2015.
    • 2015-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo61934

  • Mechanical properties of graphene nanoplatelet/carbon fiber/epoxy hybrid composites : multiscale modeling and experiments / C.M. Hadden [and seven others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, June 2015.
    • 2015-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo64630

  • Prediction of composite laminate fracture : micromechanics and progressive fracture / P.K. Gotsis and C.C. Chamis, L. Minnetyan.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, December 1996.
    • 1996-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo70378

  • Multiscale static analysis of notched and unnotched laminates using the generalized method of cells / Paria Naghipour Ghezeljeh [and six others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, August 2016.
    • 2016-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71786

  • Properties of two carbon composite materials using LTM25 epoxy resin / Juan R. Cruz, C.H. Shah and A.S. Postyn.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, November 1996.
    • 1996-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS67209

  • The impact response of carbon/epoxy laminates / A.T. Nettles and A.J. Hodge.

    • Text
    • Marshall Space Flight Center, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, November 1997.
    • 1997-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo79004

  • A progressive damage methodology for residual strength predictions of notched composite panels / Timothy W. Coats and Charles E. Harris.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, June 1998.
    • 1998-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo83019

  • Low velocity instrumented impact testing of four new damage tolerant carbon/epoxy composite systems / D.G. Lance and A.T. Nettles.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, VA : For sale by the National Technical Information Service, 1990.
    • 1990
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS60878

  • Progressive damage analysis of bonded composite joints / Frank A. Leone, Jr., Donato Girolamo, Carlos G. Dávila.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo37682

  • A test for characterizing delamination migration in carbon/epoxy tape laminates / James G. Ratcliffe, Michael W. Czabaj and Thomas K. O'Brien.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 2013.
    • 2013-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo54339

  • A damage resistance comparison of wet-wound IM7 and T1100 carbon fiber/epoxy cylinders / A.T. Nettles and A.M. Clark.

    • Text
    • Huntsville, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, April 2022.
    • 2022-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo177589

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