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The initial buckling strength of composite plate arrays with novel planform configurations are evaluated for combinations of uniform in-plane compression and shear loading and are presented in the form of dimensionless buckling interaction curves, for direct comparison with isotropic panels of equal mass. Results illustrate the buckling strength sensitivity with respect to changes in the stacking sequence of symmetric, specially orthotropic angle-ply composite laminates including the consideration of both cross-symmetric and non-symmetric
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C.B. York (2007) studied this question.
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