Abstract
The buckling strength and behavior of the simply-supported rectangular FRP plate with a centrally located hole under uniaxial and biaxial compressive loading is elucidated as the numerical results of FEM. The composite materials consisting of carbon-fiber/epoxy are treated as the case of angle-ply and cross-ply orthotropic laminates.
Cite
CITATION STYLE
APA
Yasui, Y. (1992). The buckling of Rectangular Composite Plates with Cutout under Uniaxial and Biaxial Compression. Advanced Composites Letters, 1(1). https://doi.org/10.1177/096369359200100104
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