Abstract
In this paper, the effect of the skin configuration on the buckling behavior of stiffened composite panels subjected to uniaxial compression was numerically and experimentally investigated. P-version finite element models containing all the structural details were used to predict the buckling load and buckling mode of stiffened composite panels. The upper and lower ends of the panel were fixed by potting a tin bismuth alloy with melting temperature around 70 °C to get an uniformly loading condition in the test. The alloy could be easily recycled by heating and reutilized later for potting the other test specimens.
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