An experimental and numerical study on omega stringer debonding

Author:

Bertolini Julien,Castanié Bruno,Barrau Jean-Jacques,Navarro Jean-Philippe

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference19 articles.

1. POSICOSS-improved post-buckling simulation for design of fibre composite stiffened fuselage structures;Zimmermann;Compos Struct,2006

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

3. Degenhardt R, Zimmermann R, Rolfes R, Rohwer K. Improved material exploitation of composite airframe structures by accurate simulation of postbuckling and collapse – The projects POSICOSS and COCOMAT. AIAC-11.2005.

4. Stevens KA, Ricci R, Davies GAO. Postbuckling failure of composite compression panels. In: ICAS proceedings 1994, 19th congress of the international council of the aeronautical sciences, Anaheim, CA, vol. 3. Washington, DC: AIAA; 1994. p. 2975–81.

5. Rib separation in postbuckling stiffened shear panels;Sheppart;Compos Struct,1998

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