Constitutive Model for a Fiber Tow Bridging a Delamination Crack
Author:
Publisher
Informa UK Limited
Subject
Ceramics and Composites
Link
http://www.tandfonline.com/doi/pdf/10.1080/107594199305584
Reference27 articles.
1. P. J. Smith and R. D. Wilson. Damage Tolerant Composite Wing Panels for Transport Aircraft, Boeing Commercial Airplane Company, NASA Contractor Rep. 3951, 1985.
2. Improving the delamination resistance of CFRP by stitching—a review
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