Stiffened plates and cylindrical shells under interactive buckling
暂无分享,去创建一个
[1] Srinivasan Sridharan,et al. Mode interaction analysis of stiffened shells using “locally buckled” elements , 1994 .
[2] Srinivasan Sridharan,et al. Doubly symmetric interactive buckling of plate structures , 1983 .
[3] Srinivasan Sridharan,et al. Performance of axially compressed stiffened panels , 1989 .
[4] Viggo Tvergaard,et al. Influence of post-buckling behaviour on optimum design of stiffened panels , 1973 .
[5] Srinivasan Sridharan,et al. Modal interaction in composite cylinders under hydrostatic pressure , 1995 .
[6] D. Griffin,et al. Finite-Element Analysis , 1975 .
[7] Srinivasan Sridharan,et al. A versatile model for interactive buckling of columns and beam-columns , 1988 .
[8] A. van der Neut. The sensitivity of thin-walled compression members to column axis imperfection , 1972 .
[9] Srinivasan Sridharan,et al. An improved interactive buckling analysis of thin-walled columns having doubly symmetric sections , 1986 .
[10] M. Crisfield. A FAST INCREMENTAL/ITERATIVE SOLUTION PROCEDURE THAT HANDLES "SNAP-THROUGH" , 1981 .
[11] Srinivasan Sridharan,et al. Postbuckling response of stiffened composite cylindrical shells , 1992 .
[12] Esben Byskov,et al. Mode interaction in axially stiffened cylindrical shells , 1977 .
[13] Giles W Hunt,et al. Imperfection-sensitivity of semi-symmetric branching , 1977, Proceedings of the Royal Society of London. A. Mathematical and Physical Sciences.
[14] Srinivasan Sridharan,et al. Postbuckling analysis of layered composites using p-version finite strips , 1992 .
[15] J. M. T. Thompson,et al. On the optimum design of thin-walled compression members , 1972 .
[16] Bernard Budiansky,et al. Buckling of Structures , 1976 .
[17] Srinivasan Sridharan,et al. Interactive Buckling in Thin‐Walled Beam‐Columns , 1985 .
[18] Srinivasan Sridharan,et al. Interactive buckling analysis with finite strips , 1985 .
[19] Bernard Budiansky,et al. DYNAMIC BUCKLING OF ELASTIC STRUCTURES: CRITERIA AND ESTIMATES**This work was supported in part by the National Aeronautics and Space Administration under Grant NsG-559, and by the Division of Engineering and Applied Physics, Harvard University , 1967 .