The buckling and post-buckling behavior of curved cylindrical stringer-stiffened laminated composite and metal panels had been investigated both numerically and experimentally. The results were compared to those of cylindrical stringer-stiffened laminated composite shells to yield a way of determining the optimal structure to be used for axial compression loading. For the present tested structures, the composite panels showed the best load-weight ratio.
Behavior of curved laminated composite panels and shells under axial compression
2015
Aufsatz (Zeitschrift)
Englisch
Buckling Behavior of Composite Laminated Stiffened Panels Under Combined Shear-Axial Compression
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|Postbuckling Analysis of Composite Laminated Cylindrical Panels Under Axial Compression (TN)
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