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

BISAGNI, CHIARA
2015

Abstract

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.
Buckling tests; Curved cylindrical panels; Shell structures; Post-buckling behavior; Collapse
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11311/964081
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