Buckling Analysis of Symmetrically Laminated Composite Plates

대칭복합적층평판의 좌굴해석

  • Published : 1997.10.01

Abstract

The experimental and numerical results of buckling loads for symmetrically laminated composite plates are compared. Boundary conditions are all fixed supports. Experiments were conducted for plates with fiber angles $\theta$=30$^{\circ}$, 45$^{\circ}$, 60$^{\circ}$ and aspect ratios a/b=0.8. Experimental results were obtained from load-deflection curves. Numerical methods were presented to evaluate buckling loads, using structural analysis results from ANSYS.

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