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ABSTRACT
Calculation of Energy Release Rate in Mode I Delamination of Angle Ply Laminated Composites
The International Conference on Computational & Experimental Engineering and Sciences 2007, 1(2), 61-68. https://doi.org/10.3970/icces.2007.001.061
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The compliance equation is used to calculate the energy release rate for angle ply laminated double cantilever composite beam specimen. Instead of the traditional approach of a beam on an elastic foundation, a second order shear thickness deformation beam theory (SSTDBT) has been considered.Keywords
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APA Style
Gordnian, K., Hadavinia, H., Simpson, G., Aboutorabi, A. (2007). Calculation of energy release rate in mode I delamination of angle ply laminated composites. The International Conference on Computational & Experimental Engineering and Sciences, 1(2), 61-68. https://doi.org/10.3970/icces.2007.001.061
Vancouver Style
Gordnian K, Hadavinia H, Simpson G, Aboutorabi A. Calculation of energy release rate in mode I delamination of angle ply laminated composites. Int Conf Comput Exp Eng Sciences . 2007;1(2):61-68 https://doi.org/10.3970/icces.2007.001.061
IEEE Style
K. Gordnian, H. Hadavinia, G. Simpson, and A. Aboutorabi, “Calculation of Energy Release Rate in Mode I Delamination of Angle Ply Laminated Composites,” Int. Conf. Comput. Exp. Eng. Sciences , vol. 1, no. 2, pp. 61-68, 2007. https://doi.org/10.3970/icces.2007.001.061
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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