Abstract

The present analysis deals with stiffened panels in which plate buckling, possibly involving torsion of the stiffeners, dominates the local buckling mode. Previous work on the post-buckling behaviour of long flat plates is employed to write reasonably simple and still sufficiently accurate expressions for the displacements in the initial post-buckling range. The concept of slowly varying functions is employed in the derivation of a relatively simple approximate energy expression governing combined local and overall buckling of the panel. In addition to the ratio of the critical stresses for overall and local buckling λE = σE/σloc energy expression depends essentially on only one additional nondimensional parameter. Moreover, the latter parameter depends only on properties of the cross-section, and it does not appear to vary widely for the cross-sections likely to be encountered in practice.

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