Comparison of 2D finite element modeling assumptions with results from 3D analysis for composite skin-stiffener debonding

Author:

Krueger Ronald,Paris Isabelle L,Kevin O'Brien T,Minguet Pierre J

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference17 articles.

1. 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

2. Analysis of test methods for characterizing skin/stringer debonding failures in reinforced composite panels;Minguet;Composite Materials: Testing and Design (Twelfth volume). ASTM STP,1996

3. Analysis of composite skin/stringer bond failures using a strain energy release rate approach;Minguet,1995

4. Minguet PJ. Analysis of the strength of the interface between frame and skin in a bonded composite fuselage panel. In: The 38th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 1997, p. 2783–90

5. Cvitkovich MK, O'Brien TK, Minguet PJ. Fatigue debonding characterization in composite skin/stringer configurations. In: Composite materials: fatigue and fracture, vol. 7. ASTM STP 1330: American Society for Testing and Materials. 1998. p. 97–121

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