On the analysis of composite structures with material and geometric non-linearities-Reference-Cited by-同舟云学术

On the analysis of composite structures with material and geometric non-linearities

Published:2000-12 Issue:4 Volume:50 Page:417-431
ISSN:0263-8223
Container-title:Composite Structures
language:en
Short-container-title:Composite Structures

Author:

Jones R.,Alesi H.

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference35 articles.

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2. Damage tolerance and fatigue evaluation of structure. Federal Aviation Administration Advisory Circular, 25.571-1A; 1986

3. Hachenberg D, Kossira H. Theoretical and experimental investigation of stringer peeling effects at stiffened shearloaded composite panels in the postbuckling range. ICAS-90-4.3.1; 1990. p. 511–21

4. Davies GAO, Robinson P. Predicting failure by debonding/delamination. Dept of Aeronautics, Imperial College, London, Report on Brite Euram Programs BE 3159 & BE 3160; 1992. p. 5-1–5-28

5. Stiffener/skin interactions in pressure-loaded composite panels;Hyer;AIAA J,1989

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