Strength Prediction in Open Hole Composite Laminates by Using Discrete Damage Modeling

Title
Strength Prediction in Open Hole Composite Laminates by Using Discrete Damage Modeling
Authors
Keywords
-
Journal
AIAA JOURNAL
Volume 51, Issue 4, Pages 936-945
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Online
2013-02-19
DOI
10.2514/1.j051773

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