Buckling and postbuckling behavior of composite cross-ply laminates with multiple delaminations-Reference-Cited by-同舟云学术

Buckling and postbuckling behavior of composite cross-ply laminates with multiple delaminations

Published:1998-12 Issue:4 Volume:43 Page:257-274
ISSN:0263-8223
Container-title:Composite Structures
language:en
Short-container-title:Composite Structures

Author:

Kyoung Woo-Min,Kim Chun-Gon,Hong Chang-Sun

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference18 articles.

1. Impact-induced delamination — a view of bending stiffness mismatching;Liu;J Composite Mater,1988

2. The influence of lay-up and thickness on composite impact damage and compression strength;Guynn,1985

3. Experimental analysis on residual compressive strength of graphite/epoxy and graphite/PEEK composite laminates after low-velocity impact;Choi;J KSCM,1993

4. One-dimensional modeling of failure in laminates plates by delamination buckling;Chai;Int J Solids Structures,1981

5. Effect of delamination of axially loaded homogeneous laminates plates;Simitses;AIAA J,1985

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