Analysis of composite skin–stiffener debond specimens using a shell/3D modeling technique

Author:

Krueger Ronald,Minguet Pierre J.

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference33 articles.

1. Fracture mechanics analyses for skin–stiffener debonding;Raju;Eng Fract Mech,1996

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

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

4. 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.

5. Minguet PJ, O’Brien TK. Analysis of composite skin/stringer bond failures using a strain energy release rate approach. In: Poursartip A, Street K, editors. The tenth international conference on composite materials, vol. I, 1995. p. 245–52.

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