Mode I Interlaminar Fracture Toughness of Composites Using Slender Double Cantilevered Beam Specimens
Author:
Affiliation:
1. Boeing Commercial Airplane Company P.O. Box 3707 M/S 6C-11 Seattle, WA 98124
2. Photon Kinetics S W Cirrus Beaverton, OR 97075
3. Morton Thiokol Inc. P.O. Box 524 M/S 287E Brigham City, UT 84302
Abstract
Publisher
SAGE Publications
Subject
Materials Chemistry,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites
Link
http://journals.sagepub.com/doi/pdf/10.1177/002199838501900204
Reference47 articles.
1. The interlaminar fracture of organic-matrix, woven reinforcement composites
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