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  • Strain rate dependent modeling of polymer matrix composites [microform] / Robert K. Goldberg, Donald C. Stouffer.

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

  • Isothermal fatigue behavior of a [90]₈ Sic/Ti-15-3 composite at 426 ⁰C [microform] / John Gayda and Timothy P. Gabb.

    • Text
    • [Washington, D.C.] : NASA ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • Laminated thin shell structures subjected to free vibration in a hygrothermal environment [microform] / Pascal K. Gotsis and James D. Guptill .

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

  • Isothermal damage and fatigue behavior and SCS-6/timetal 21S [0/90]s composite at 650̊C [microform] / Michael G. Castelli.

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

  • Thermomechanical fatigue damage/failure mechanisms in SCS-6/timetal 21S [0/90]s composite [microform] / Michael G. Castelli.

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

  • 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

  • Innovative design of composite structures [microform] : use of curvilinear fiber format to improve structural efficiency / M.W. Hyer, R.F. Charette.

    • Text
    • College Park, MD : Dept. of Mechanical Engineering, University of Maryland ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • Impact damage resistance and residual property assessment of [0/+/-45/90]s SCS-6/Timetal 21S [microform] / Jennifer L. Miller, Marc A. Portanova, W. Steven Johnson.

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

  • Influence of fiber architecture on the elastic and inelastic response of metal matrix composites [microform] / Steven M. Arnold, Marek-Jerzy Pindera, and Thomas E. Wilt.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [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

  • Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation [microform] / William L. Ko.

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

  • Design protocols and analytical strategies that incorporate structural reliability models [microform] : final report; reporting period: January 19, 1996 - January 18, 1997; grant number: NASA cooperative agreement NCC 3-448 / principal investigator, Stephen F. Duffy.

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

  • Two-color laser speckle shift strain measurement system [microform] / Margaret L. Tuma ... [et al.].

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

  • A progressive damage methodology for residual strength predictions of center-crack tension composite panels [microform] / Timothy William Coats.

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

  • Progressive fracture of fiber composite thin shell structures under internal pressure and axial loads [microform] / Pascal K. Gotsis and Christos C. Chamis ; Levon Minnetyan.

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

  • Free vibration of fiber composite thin shells in a hot environment [microform] / Pascal K. Gotsis and James D. Guptill.

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

  • High strain rate deformation modeling of a polymer matrix composite [microform] / Robert K. Goldberg, Donald C. Stouffer.

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

  • High strain rate deformation modeling of a polymer matrix composite [microform] / Robert K. Goldberg, Donald C. Stouffer.

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

  • Strain rate dependent deformation and strength modeling of a polymer matrix composite utilizing a micromechanics approach [microform] / Robert K. Goldberg.

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

  • Fatigue crack growth in unidirectional metal matrix composite [microform] / Louis J. Ghosn, Jack Telesman and Peter Kantzos ; prepared for the International Fatigue Series (FATIGUE 90), Honolulu, Hawaii, July 15-20, 1990.

    • 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/LPS61905

  • 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

  • Innovative design of composite structures [microform] : the use of curvilinear fiber format to improve buckling resistance of composite plates with central circular holes / M.W. Hyer, H.H. Lee.

    • Text
    • Blacksburg, VA : College of Engineering, Virginia Polytechnic Institute and State University ; [Washington, D.C. : National Aeronautics and Space Administration, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67540

  • Innovative design of composite structures [microform] : the use of curvilinear fiber format in composite structure design / M.W. Hyer, R.F. Charette.

    • Text
    • Blacksburg, VA : College of Engineering, Virginia Polytechnic Institute and State University ; [Washington, D.C. : National Aeronautics and Space Administration, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS67541

  • Structural behavior of composites with progressive fracture [microform] / Levon Minnetyan, Christos C. Chamis, and Pappu L.N. Murthy.

    • 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/LPS68983

  • A comparison of the Bromination dynamics of pitch-based and vapor-grown graphite fibers [microform] / James E. Gaier.

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
    • 1986

  • A simple approach to determination of stiffness characteristics of unidirectional composites [microform] / Zhao, Jian-hua.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, [1983]
    • 1983

  • Numerical implementation of a multiple-ISV thermodynamically-based work potential theory for modeling progressive damage and failure in fiber-reinforced laminates / Evan J. Pineda, Anthony M. Waas.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo24418

  • Simple theoretical models for composite rotor blades / R. Rao Valisetty and Lawrence W. Rehfield.

    • Text
    • Atlanta, Georgia : Georgia Institute of Technology. : School of Aerospace Engineering ; [Washington, DC] : National Aeronautics and Space Administration, 1984.
    • 1984
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo46535

  • Simple theoretical models for composite rotor blades / R. Rao Valisetty and Lawrence W. Rehfield.

    • Text
    • Atlanta, Georgia : Georgia Institute of Technology : School of Aerospace Engineering ; [Washington, DC] : National Aeronautics and Space Administration, 1984.
    • 1984

  • Progressive fracture of fiber composite thin shell structures under internal pressure and axial loads / Pascal K. Gotsis and Christos C. Chamis, Levon Minnetyan.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, September 1996.
    • 1996-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo69196

  • Two-color laser speckle shift strain measurement system / Margaret L. Tuma [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, August 1996.
    • 1996-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo70064

  • Design and manufacture of elastically tailored tow placed plates / Brian F. Tatting, Zafer Gürdal.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. :] : [For sale by the National Technical Information Service], [2002]
    • 2002
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS60511

  • Utilization of the generalized method of cells to analyze the deformation response of laminated ceramic matrix composites / Robert K. Goldberg.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo38101

  • The effect of general statistical fiber misalignment on predicted damage initiation in composites / Brett A. Bednarcyk, Jacob Aboudi, Steven M. Arnold.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2014.
    • 2014-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo56909

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