Effect of trapezoidal shapes and non-uniform edge loads on buckling behaviour of plates with cutouts
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DOI: 10.1177/09544062211022258
Abstract: Crucial buckling loads of composite laminates are typically determined by employing analytical techniques based on the presumptions that the plates are susceptible to uniform edge loads, ignoring the fact that the practical assemblies are regularly… read more here.
Keywords: uniform edge; buckling behaviour; panel; non uniform ... See more keywords