Research Catalog

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  • A method for calculating strain energy release rates in preliminary design of composite skin/stringer debonding under multi-axial loading [microform] / Ronald Krueger, Pierre J. Minguet, T. Kevin O'Brien.

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

  • Implementation of equivalent domain integral method in the two-dimensional analysis of mixed mode problems [microform] / I.S. Raju and K.N. Shivakumar.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • The evolution and growth of Al₂O₃ scales on β-NiAl [microform] / by Joseph Doychak.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • The influence of defects on the fatigue resistance of butt and girth welds in A106B steel [microform] / B.N. Leis, D.P. Goetz, and P.M. Scott.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1986]
    • 1986

  • Fatigue-life prediction methodology using small-crack theory [microform] / J.C. Newman, Jr. and E.P. Phillips, M.H. Swain.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • FASTRAN-II [microform] : a fatigue crack growth structural analysis program / J.C. Newman, Jr.

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

  • The merging of fatigue and fracture mechanics concepts [microform] : a historical perspective / J.C. Newman, Jr.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Stress ratio effects on crack opening loads and crack growth rates in aluminum alloy 2024 [microform] / William T. Riddell and Robert S. Piascik.

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

  • Through-the-thickness fatigue crack closure behavior in an aluminum alloy [microform] / D.S. Dawicke, J.C. Newman, Jr., and A.F. Grandt, Jr.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS62877

  • Influence of fatigue crack wake length and state of stress and on crack closure [microform] / Jack Telesman and Douglas M. Fisher.

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

  • Variables controlling fatigue crack growth of short cracks [microform] / Jack Telesman and Douglas M. Fisher, and Donna Holka.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS85238

  • Three-dimensional measurements of fatigue crack closure [microform] : semi-annual status report / submitted by A.F. Grandt, Jr.

    • Text
    • [Washington, D.C.? : National Aeronautics and Space Administration, 1984]
    • 1984

  • Results of the round robin on opening-load measurement [microform] : conducted by ASTM Task Group E24.04.04 on crack closure measurement and analysis / Edward P. Phillips.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS93125

  • Development and application of benchmark examples for mode II static delamination propagation and fatigue growth predictions / Ronald Krueger.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center : National Institute of Aerospace, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo23295

  • Mitigation of crack damage in metallic materials / Patrick Leser [and seven others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, May 2014.
    • 2014-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo52361

  • Floating node method and virtual crack closure technique for modeling matrix cracking-delamination interaction / N.V. De Carvalho [and five others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, July 2013.
    • 2013-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo53799

  • Fatigue resistance of liquid-assisted self-repairing aluminum alloys reinforced with shape memory alloys : Shape Memory Alloy Self-Healing (SMASH) technology for aeronautical applications / M. Clara Wright, Dr. Michele Manuel, Dr. Terryl Wallace.

    • Text
    • [Cocoa Beach, FL] : [NASA Kennedy Space Center], September 2013.
    • 2013-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo54681

  • Development and application of benchmark examples for mixed-mode I/II quasi-static delamination propagation predictions / Ronald Krueger.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, April 2012.
    • 2012-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo32908

  • An enriched shell finite element for progressive damage simulation in composite laminates / Mark W. McElroy.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, June 2016.
    • 2016-6
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo77403

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