Nonlinear Theory for Composite Laminated Shells With Interfacial Damage
Author:
Affiliation:
1. Department of Modern Mechanics, University of Science and Technology of China Hefei, Anhui 230026, P. R. China
2. Department of Civil Engineering, The University of Queensland, Brisbane, QLD 4072, Australia
Abstract
Publisher
ASME International
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics
Link
http://asmedigitalcollection.asme.org/appliedmechanics/article-pdf/65/3/711/5465511/711_1.pdf
Reference34 articles.
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2. Achenbach J. D. , and ZhuH., 1989, “Effect of interfacial zone on mechanical behaviour and failure of fibre-reinforced composites,” Journal of the Mechanics and Physics of Solids, Vol. 37, pp. 381–393.
3. Benveniste, Y., and Dvorak, G. J., 1990, “On a correspondence between mechanical and thermal fields with slipping interfaces,” Inelastic Deformation of Composite Materials (IUTAM Symposium), G. J. Dvorak ed., Springer-Verlag, New York, pp. 77–98.
4. Cheng Z. Q. , HowsonW. P., and WilliamsF. W., 1997, “Modelling of weakly bonded laminated composite plates at large deflections,” International Journal of Solids and Structures, Vol. 34, pp. 3583–3599.
5. Cheng Z. Q. , JemahA. K., and WilliamsF. W., 1996a, “Theory for multilayered anisotropic plates with weakened interfaces,” ASME JOURNAL OF APPLIED MECHANICS, Vol. 63, pp. 1019–1026.
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