NASA NTRS ยท 19850004959
A buckling analysis for rectangular orthotropic plates with centrally located cutouts
Abstract
An analysis to obtain the buckling loads of a rectangular orthotropic plate with a centrally located cutout is described. Cutout shapes can be elliptical, circular, rectangular, or square. The boundary conditions considered in the analysis are simply supported unloaded edges and either clamped or simply supported loaded edges. The plate is loaded in uniaxial compression by either uniform edge displacement or uniform edge stress. A computer program that implements this analysis is described, and the program use is demonstrated by sample problems.
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Michael P. Nemeth. 1984-12-01. A buckling analysis for rectangular orthotropic plates with centrally located cutouts. https://ntrs.nasa.gov/citations/19850004959
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