Research Catalog

  • Axisymmetric shell analysis of the space shuttle solid rocket booster field joint [microform] / Michael P. Nemeth, Melvin S. Anderson.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1991.
    • 1991
  • Buckling behavior of long symmetrically laminated plates subjected to combined loadings [microform] / Michael P. Nemeth.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1992.
    • 1992
  • Nondimensional parameters and equations for buckling of symmetrically laminated thin elastic shallow shells [microform] / Michael P. Nemeth.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991
  • Buckling behavior of long anisotropic plates subjected to combined loads [microform] / Michael P. Nemeth.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Buckling behavior of long symmetrically laminated plates subjected to shear and linearly varying axial edge loads [microform] / Michael P. Nemeth.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997
  • Buckling behavior of long anisotropic plates subjected to combined loads [microform] / Michael P. Nemeth.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Buckling and postbuckling behavior of laminated composite plates with a cutout [microform] / Michael P. Nemeth.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • The NASA monographs on shell stability design recommendations [microform] : a review and suggested improvements / Michael P. Nemeth and James H. Starnes, Jr.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998
  • Buckling and postbuckling behavior of compression-loaded isotropic plates with cutouts [microform] / Michael P. Nemeth.

    • 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/LPS65434
  • An in-depth tutorial on constitutive equations for elastic anisotropic materials / Michael P. Nemeth.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo22688
  • Cubic zig-zag enrichment of the classical Kirchhoff kinematics for laminated and sandwich plates / Michael P. Nemeth.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo28057
  • Conditions for symmetries in the buckle patterns of laminated-composite plates / Michael P. Nemeth.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo30943
  • An Approximate solution and master curves for buckling of symmetrically laminated composite cylinders / Michael P. Nemeth.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo45682
  • Buckling analysis for stiffened anisotropic circular cylinders based on Sanders' nonlinear shell theory / Michael P. Nemeth.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, March 2014.
    • 2014-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo55308
  • Buckling behavior of long anisotropic plates subjected to combined loads / Michael P. Nemeth.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [1996]
    • 1996
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo79372
  • 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
  • Nonlinear analysis of the space shuttle super-lightweight external fuel tank / Michael P. Nemeth [and three others].

    • Text
    • [Washington, D.C.] : [National Aeronautics and Space Administration], [April 1996]
    • 1996-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo177262
  • Buckling behavior of long symmetrically laminated plates subjected to combined loadings / Michael P. Nemeth.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, May 1992.
    • 1992-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo195860

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