Stress analysis of a mode I edge delamination specimen for compositematerials
- 1 July 1986
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 24 (7) , 1163-1168
- https://doi.org/10.2514/3.9408
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
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- A Refined Theory of Elastic, Orthotropic PlatesJournal of Applied Mechanics, 1958