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  • Uniaxial stretching of poly(keto-ether-imide) films [microform] / Jeffrey A. Hinkley ... [et al.].

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

  • Elevated temperature axial and torsional fatigue behavior of Haynes 188 [microform] / Peter J. Bonacuse, Sreeramesh Kalluri.

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

  • Stability limits and dynamics of nonaxisymmetric liquid bridges [microform] : final report / prepared by J. Iwan D. Alexander, principal investigator.

    • Text
    • Huntsville, AL : Center for Microgravity and Materials Research, University of Alabama in Huntsville ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • An axial-torsional, thermomechanical fatigue testing technique [microform] / Sreeramesh Kalluri and Peter J. Bonacuse.

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

  • HOTCFGM-1D [microform] : a coupled higher-order theory for cylindrical structural components with through-thickness functionally graded microstructures / Marek-Jerzy Pindera, Jacob Aboudi.

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

  • An analysis of the macroscopic tensile behavior of a nonlinear nylon reinforced elastomeric composite system using MAC/GMC [microform] / Mahmoud Assaad, Steven M. Arnold.

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

  • Analysis of interlaminar stresses in thick composite laminates with and without edge delamination [microform] / John D. Whitcomb and I. S. Raju.

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

  • A data acquisition and control program for axial-torsional fatigue testing [electronic resource] / Sreeramesh Kalluri and Peter J. Bonacuse.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [St. Louis Mo. : US Army Aviation Systems Command, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS107748

  • A data acquisition and control program for axial-torsional fatigue testing [microform] / Sreeramesh Kalluri and Peter J. Bonacuse.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [St. Louis Mo. : US Army Aviation Systems Command, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS107748

  • Buckling test results from the 8-foot-diameter orthogrid-stiffened cylinder test article TA01 : test dates: 19-21 November 2008 / Mark W. Hilburger, W. Allen Waters, Jr., Waddy T. Haynie.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 2015.
    • 2015-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo62964

  • The exact solution for linear thermoelastic axisymmetric deformations of generally laminated circular cylindrical shells / Michael P. Nemeth and Marc R. Schultz.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo33345

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