Post-buckling Behaviour of Imperfect Cylindrical Panels Subjected to Axial Compressive Load: Experimental vs.Theoretical

Author:

RamanaReddy D.V.,Gunda Jagadish Babu,Padal K.T. Balaram

Publisher

Elsevier BV

Subject

General Medicine

Reference12 articles.

1. Koiter, W.T., 1955. Buckling and Post Buckling behavior of a cylindrical panel under axial compression, National aeronautical research institute. Amsterdam, Report S.476, C. C. L, Class. C- 473–1.

2. Sabir, B., Lock A.C., 1972. The Application of Finite Elements to the Large-deflection Geometrically Nonlinear Behavior of Cylindrical Shells. Proceedings of International Conference on Variational Mechanics. Southampton University, Session VII.

3. Analysis of unbraced multistory steel rigid frames;Wright;International Journal of Structural Division ASCE,1968

4. Bergan, P.G., Soreide, T.H., 1978. Solution of Large Displacement and Instability Problems Using the Current stiffness Parameter. In: Finite Element in Nonlinear.

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