NASA NTRS · 19760000111
BUCLAP2
Abstract
Program is used to predict buckling of rectangular flat and curved laminated plates subjected to in-plane normal and shearing loads, with each lamina composed of orthotropic material with arbitrary orientation of orthotropic axes.
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Halstead, D. W., Tripp, L. L., Tamekuni, M., Baker, L. L., Viswanathan, A. V.. 1976-03-01. BUCLAP2. https://ntrs.nasa.gov/citations/19760000111
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