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  • Laminated thin shell structures subjected to free vibration in a hygrothermal environment [microform] / Pascal K. Gotsis and James D. Guptill .

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Neotectonics of Asia [microform] : thin-shell finite-element models with faults / by Xianghong Kong and Peter Bird.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • The inviscid axisymmetric stability of the supersonic flow along a circular cylinder [microform] / Peter W. Duck.

    • Text
    • Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • A technical report entitled Formulation of the nonlinear analysis of shell-like structures, subjected to time-dependent mechanical and thermal loading [microform] / by George J. Simitses, Robert L. Carlson, and Richard Riff.

    • Text
    • Atlanta, Ga. : Georgia Institute of Technology, School of Engineering Science and Mechanics ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986?]
    • 1986

  • Nonlinear analysis of thin fracture specimens using solid, isoparametric finite elements [microform] / Carlos G. Matos and Robert H. Dodds, Jr.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Global dynamic modeling of space-geodetic data [microform] : final report, NASA award NAGW-3042, 1 Jan. 1992 to 31 Dec. 1995 / Peter Bird.

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

  • The influence of lamination angles on the interior noise levels of an aircraft [microform] / Christian M. Fernholz, Jay H. Robinson.

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

  • Computational simulation of damage progression of composite thin shells subjected to mechanical loads [microform] / P.K. Gotsis, C.C. Chamis, L. Minnetyan.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • LQR control of thin shell dynamics [microform] : formulation and numerical implementation / R.C.H. del Rosario and R.C. Smith.

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

  • 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

  • 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

  • Progressive fracture of fiber composite thin shell structures under internal pressure and axial loads [microform] / Pascal K. Gotsis and Christos C. Chamis ; Levon Minnetyan.

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

  • Free vibration of fiber composite thin shells in a hot environment [microform] / Pascal K. Gotsis and James D. Guptill.

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

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

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, [1988]
    • 1988
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS112015

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

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, [1988]
    • 1988

  • The influence of lamination angles on the interior noise levels of an aircraft / Christian M. Fernholz, Jay H. Robinson.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 1996.
    • 1996-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo67749

  • 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

  • Axial-torsional fatigue : a study of tubular specimen thickness effects / Peter J. Bonacuse and Sreeramesh Kalluri.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, December 1990.
    • 1990-12

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