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  • Hierarchic plate and shell models based on p-extension [microform] / Barna A. Szabó, Glenn J. Sahrmann.

    • Text
    • St. Louis, MO : Center for Computational Mechanics, Washington University ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • A three-node C̊ element for analysis of laminated composite sandwich shells [microform] / C. Wayne Martin, S.F. Lung, and K.K. Gupta.

    • 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, 1989.
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS96605

  • Analysis of shell-type structures subjected to time-dependent mechanical and thermal loading [electronic resource] : a semi-annual status report submitted to NASA-Lewis Research Center, Cleveland, Ohio / by G.J. Simitses, R.L. Carlson, and R. Riff.

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1987]
    • 1987
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS113255

  • Analysis of shell-type structures subjected to time-dependent mechanical and thermal loading [microform] : a semi-annual status report submitted to NASA-Lewis Research Center, Cleveland, Ohio / by G.J. Simitses, R.L. Carlson, and R. Riff.

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1987]
    • 1987
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS113255

  • Plates and shells containing a surface crack under general loading conditions [microform] / Paul F. Joseph and Fazil Erdogan.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1987]
    • 1987

  • Loft : an automated mesh generator for stiffened shell aerospace vehicles / Lloyd B. Eldred.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo22678

  • Analysis of shell-type structures subjected to time-dependent mechanical and thermal loading : a semi-annual status report / by G.J. Simitses.

    • Text
    • Cleveland, Ohio : NASA Lewis Research Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo30983

  • Analysis of shell-type structures subjected to time-dependent mechanical and thermal loading [microform] : a semi-annual status report / by G.J. Simitses.

    • Text
    • Cleveland, Ohio : NASA Lewis Research Center, [1989]
    • 1989

  • On hybrid and mixed finite element methods / Th. H.H. Pian.

    • Text
    • Cambridge, Massachusetts : Massachusetts Institute of Technology ; [Washington, DC] : National Aeronautics and Space Administration, 1981.
    • 1981
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo46542

  • On hybrid and mixed finite element methods / Th. H.H. Pian.

    • Text
    • Cambridge, Massachusetts : Massachusetts Institute of Technology ; [Washington, DC] : National Aeronautics and Space Administration, 1981.
    • 1981

  • Recent advances in hybrid/mixed finite elements / Theodore H.H. Pian.

    • Text
    • [Place of publication not identified] : Cambridge, Mass. : Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, [1985]
    • 1985
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo35591

  • Verification of orthogrid finite element modeling techniques / B.E. Steeve.

    • Text
    • MSFC, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, October 1996.
    • 1996-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo67652

  • 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

  • Composite Crew Module (CCM) permeability characterization / Michael T. Kirsch.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo41418

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