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  1. 1
    A Probabilistic method for the buckling assessment of stiffened composite shells

    A Probabilistic method for the buckling assessment of stiffened composite shells

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1993
    Format: Government Document Book


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  2. 2
    Strain-energy release rate analysis of a laminate with a postbuckled delamination

    Strain-energy release rate analysis of a laminate with a postbuckled delamination by Whitcomb, J. D.

    Format: Government Document Book


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  3. 3
    Buckling of simply supported plywood plates under combined edgewise bending and compression

    Buckling of simply supported plywood plates under combined edgewise bending and compression by Zahn, John J., 1932-

    Madison, Wis. : U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory, 1965
    Format: Government Document Book


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  4. 4
    Simplified nonlinear analysis of large space-trusses and space-frames, using explicitly derived tangent stiffnesses and accounting for local buckling

    Simplified nonlinear analysis of large space-trusses and space-frames, using explicitly derived tangent stiffnesses and accounting for local buckling

    Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1985
    Format: Government Document Book


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  5. 5
    Buckle in veneer

    Buckle in veneer by Lutz, J. F. (John Francis), 1920-

    Madison, Wis. : U.S. Dept. of Agriculture, Forest Service, 1970
    Format: Government Document Book


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  6. 6
    Design methodology and life analysis of postbuckled metal and composite panels. : Volume 1 / R. B. Deo, B. L. Agarwal, E. Madenci.

    Design methodology and life analysis of postbuckled metal and composite panels. : Volume 1 / R. B. Deo, B. L. Agarwal, E. Madenci. by Deo, R. B.

    Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Materials Laboratories, Air Force Systems Command, United States Air Force, 1985
    Format: Government Document Book


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  7. 7
    Development of curved-plate elements for the exact buckling analysis of composite plate assemblies including transverse-shear effects

    Development of curved-plate elements for the exact buckling analysis of composite plate assemblies including transverse-shear effects by McGowan, David Michael

    1997
    Format: Government Document Thesis Book


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  8. 8
    Accuracies of Southwell and force/stiffness methods in the prediction of buckling strength of hypersonic aircraft wing tubular panels

    Accuracies of Southwell and force/stiffness methods in the prediction of buckling strength of hypersonic aircraft wing tubular panels by Ko, William L.

    Edwards, Calif. : [Springfield, Va. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; For sale by the National Technical Information Service], 1987
    Format: Government Document Book


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  9. 9
    Elastic stability of circular cylindrical shells

    Elastic stability of circular cylindrical shells by Yamaki, N. (Noboru), 1920-2004

    Amsterdam ; New York : New York, N.Y. : North-Holland ; Sole distributors for the U.S.A. and Canada, Elsevier Science Pub. Co., 1984
    Format: Book


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  10. 10
    Column stiffener detailing and panel zone behavior of steel moment frame connections

    Column stiffener detailing and panel zone behavior of steel moment frame connections by Cotton, Sean Carlos

    2001
    Format: Thesis Book


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  11. 11
    Local buckling and crippling of composite stiffener sections

    Local buckling and crippling of composite stiffener sections by Bonanni, David Louis, 1963-

    Blacksburg, Va. : College of Engineering, Virginia Polytechnic Institute and State University, 1988
    Format: Government Document Book


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  12. 12
    Elastic instability phenomena

    Elastic instability phenomena by Thompson, J. M. T.

    Chichester ; New York : Wiley, 1984
    Format: Book


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  13. 13
    Extension of the safe geometric parameters to slightly enriched uranium

    Extension of the safe geometric parameters to slightly enriched uranium by Newlon, C. E.

    Oak Ridge, Tenn. : Union Carbide Nuclear Company, Oak Ridge Gaseous Diffusion Plant, 1958
    Format: Government Document Book


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  14. 14
    The buckling of plates and shells

    The buckling of plates and shells by Cox, H. L. (Harold Leslie)

    Oxford, New York : Pergamon Press, 1963
    Format: Book


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  15. 15
    Reliability of shell buckling predictions

    Reliability of shell buckling predictions by Litle, William A.

    Cambridge, Mass. : M.I.T. Press, 1964
    Format: Book


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  16. 16
    Buckling experiments : experimental methods in buckling of thin-walled structures

    Buckling experiments : experimental methods in buckling of thin-walled structures by Singer, J.

    Chichester ; New York : Wiley, 1998
    Format: Book


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  17. 17
    User manual for VICONOPT : an exact analysis and optimum design program covering the buckling and vibration of prismatic assemblies of flat in-plane loaded, anisotropic plates with approximations for discrete supports and transverse stiffeners

    User manual for VICONOPT : an exact analysis and optimum design program covering the buckling and vibration of prismatic assemblies of flat in-plane loaded, anisotropic plates with... by Williams, F. W. (Frederick Wallace), 1939-

    Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1990
    Format: Government Document Book


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  18. 18
    Optimal design of geodesically stiffened composite cylindrical shells

    Optimal design of geodesically stiffened composite cylindrical shells by Gendron, G.

    Blacksburg, Va. : [Washington, DC] : [Springfield, Va.] : College of Engineering, Virginia Polytechnic Institute and State University ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1992
    Format: Government Document Book


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  19. 19
    Evaluation of MHOST analysis capabilities for a plate element

    Evaluation of MHOST analysis capabilities for a plate element by Lee, Ho-Jun

    [Washington, DC] : National Aeronautics and Space Administration, 1992
    Format: Government Document Book


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  20. 20
    Buckling and vibration analysis of a simply supported column with a piecewise constant cross section

    Buckling and vibration analysis of a simply supported column with a piecewise constant cross section by Lake, Mark S.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1991
    Format: Government Document Book


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