Application of Analytic Models for Thin Embedded Delamination Buckling in Composite Material Panels

Author:

Lucariello D.,Di Caprio F.,Borelli R.,Mercurio U.

Publisher

Springer Science and Business Media LLC

Reference35 articles.

1. K.N. Shivakumar, J. D. Whitcomb, “Buckling of a sublaminate in quasi-isotropic composite laminate”, NASA, TM-85755, 1984.

2. J. D. Whitcomb, “Instability-related Delamination Growth of Embedded and Edge Delaminations”, NASA, TN-100655, 1988.

3. J. D. Whitcomb, “Three-Dimensional Analysis of a Post-buckled Embedded Delamination”, NASA, TP-2823, 1988.

4. H. Kim, “Postbuckling Analysis of Composite Laminates With a Delamination”, Computers and Structures, Vol.62 n.6, 1997.

5. H. Kim, C. Hong, “Buckling and Postbuckling Behavior of Composite Laminates with a Delamination”, Composites Science and Technology, Vol. 57, 1997.

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