The research here presented shows the numerical results for progressive failure of stiffened
composite panels into the post-buckling field. In particular, a strength reduction procedure is
implemented in the commercial finite element code ABAQUS where the stiffness properties of the
material are removed in the failed areas. The results show a good correlation with experimental data
obtained from a post-buckling test of a stiffened panel with a notch, that can be found in
literature.
Cite This Article
Bisagni, C. (2007). Numerical Analysis of Composite Panels in the Post-Buckling Field taking into account Progressive Failure. The International Conference on Computational & Experimental Engineering and Sciences, 1(3), 93–98. https://doi.org/10.3970/icces.2007.001.093
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