An analysis methodology for failure in postbuckling skin–stiffener interfaces

Author:

Orifici A.C.,Thomson R.S.,Herszberg I.,Weller T.,Degenhardt R.,Bayandor J.

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference14 articles.

1. COCOMAT – improved material exploitation of composite airframe structures by accurate simulation of postbuckling and collapse;Degenhardt;Compos Struct,2006

2. COCOMAT Home Page. www.cocomat.de; 2007.

3. Orifici AC, Herszberg I, Thomson RS, Weller T, Kotler A, Bayandor J. Failure in stringer interfaces in postbuckled composite stiffened panels. In: Proceedings of the 12th Australian international aerospace congress; 2007.

4. Orifici AC. Degradation models for the collapse analysis of composite aerospace structures. PhD thesis, Royal Melbourne Institute of Technology; 2007.

5. MSC.Marc User Manuals Version 2005r3. Santa Ana, CA: MSC. Software Corporation; 2006.

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