Research Catalog

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  • Closed-form static analysis with inertia relief and displacement-dependent loads using a MSC/NASTRAN DMAP alter [microform] / Alan R. Barnett and Timothy W. Widrick, Damian R. Ludwiczak.

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

  • Mode I delamination growth in adhesively bonded joints under static and fatigue loads [microform] : semi-annual report / by Subodh C. Biswas, Shaik Jeelani.

    • Text
    • Tuskegee, AL : School of Engineering and Architecture, Tuskegee University ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986?]
    • 1986

  • Some observations on the behavior of the langley model rotor blade [microform] / Lawrence W. Rehfield and Ali R. Atilgan.

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

  • Analysis of static contact in laminated composite plates using damage mechanics [microform] : final technical report / submitted by David H. Allen.

    • Text
    • Hampton, VA : NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Formulation of an improved smeared stiffener theory for buckling analysis of grid-stiffened composite panels [microform] / Navin Jaunky and Norman F. Knight, Jr., Damodar R. Ambur.

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

  • Testing for random limit load versus static limit load [microform] / H.M. Lee.

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

  • Meteorological Satellites (METSAT) and Earth Observing System (EOS), Advanced Microwave Sounding Unit-A (AMSU-A) [microform] : stress analysis report : contract no. NAS 5-32314 / submitted by Aerojet.

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

  • Quasi-static viscoelasticity loading measurements of an aircraft tire [microform] / Angela J. Mason and John A. Tanner, Arthur R. Johnson.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research 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

  • Fracture toughness and crack growth of Zerodur [microform] / Michael J. Viens.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS66849

  • Static versus dynamic loads as an influence on bone remodelling [microform] / L.E. Lanyon & C.T. Rubin.

    • Text
    • Boston, Mass. : Tufts University ; [Washington, D.C. : National Aeronautics and Space Administration, 1984]
    • 1984

  • 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

  • Application of benchmark examples to assess the single and mixed-mode static delamination propagation capabilities in ANSYS® / Ronald Krueger.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center : National Institute of Aerospace, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo31102

  • Static indentation load capacity of the superelastic 60NiTi for rolling element bearings / Christopher DellaCorte, Lewis E. Moore III and Joshua S. Clifton.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo31848

  • Structural analysis peer review for the static display of the orbiter Atlantis at the Kennedy Space Center visitors center / Stephen J. Minute.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo45680

  • Control of bone remodelling by applied dynamic loads / Lance E. Lanvon & Clinton T. Rubin.

    • Text
    • Medford, Massachusetts : Dept, of Anatomy & Cellular Biology, Tufts University, School of Veterinary Medicine ; [Washington, DC] : [National Aeronautics and Space Administration], [1984]
    • 1984
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo51595

  • Control of bone remodelling by applied dynamic loads / Lance E. Lanvon & Clinton T. Rubin.

    • Text
    • Medford, Massachusetts : Dept, of Anatomy & Cellular Biology, Tufts University, School of Veterinary Medicine ; [Washington, District of Columbia] : [National Aeronautics and Space Administration], [1984]
    • 1984

  • The effect of indenter ball radius on the static load capacity of the superelastic 60NiTi for rolling element bearings / Christopher DellaCorte, Lewis E. Moore, III and Joshua S. Clifton.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, April 2014.
    • 2014-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo52774

  • Testing for random limit load versus static limit load / H.M. Lee.

    • Text
    • MSFC, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, September 1997.
    • 1997-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo67694

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