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ABSTRACT
Numerical Analysis of Composite Panels in the Post-Buckling Field taking into account Progressive Failure
Department of Aerospace Engineering, Politecnico di Milano, Milan, Italy
The International Conference on Computational & Experimental Engineering and Sciences 2007, 1(3), 93-98. https://doi.org/10.3970/icces.2007.001.093
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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
APA Style
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
Vancouver Style
Bisagni C. Numerical analysis of composite panels in the post-buckling field taking into account progressive failure . Int Conf Comput Exp Eng Sciences . 2007;1(3):93-98 https://doi.org/10.3970/icces.2007.001.093
IEEE Style
C. Bisagni, “Numerical Analysis of Composite Panels in the Post-Buckling Field taking into account Progressive Failure ,” Int. Conf. Comput. Exp. Eng. Sciences , vol. 1, no. 3, pp. 93-98, 2007. https://doi.org/10.3970/icces.2007.001.093
Copyright © 2007 The Author(s). Published by Tech Science Press.This work is licensed under a Creative Commons Attribution 4.0 International License , which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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