Panel stiffener debonding analysis using a shell/3D modeling technique

Author:

Krueger Ronald,Ratcliffe James G.,Minguet Pierre J.

Publisher

Elsevier BV

Subject

General Engineering,Ceramics and Composites

Reference23 articles.

1. Failure of thick-skinned stiffener runout sections loaded in uniaxial compression;Falzon;Compos Struct,2001

2. The analysis of skin-to-stiffener debonding in composite aerospace structures;Yap;Compos Struct,2002

3. Minguet PJ, Fedro MJ, O’Brien TK, Martin RH, Ilcewicz LB. Development of a structural test simulating pressure pillowing effects in bonded skin/stringer/frame configuration. In: Proceedings of the fourth NASA/DoD advanced composite technology conference, Salt Lake City, Utah; 1993.

4. Minguet PJ, O’Brien TK. Analysis of test methods for characterizing skin/stringer debonding failures in reinforced composite panels. In: Composite materials: testing and design (vol. 12), ASTM STP 1274; 1996. p. 105–24.

5. Testing and analysis of composite skin/stringer debonding under multi-axial loading;Krueger;J Compos Mater,2000

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