Strain-Rate Effects on Unidirectional Carbon-Fiber Composites
Author:
Affiliation:
1. University of Michigan, Ann Arbor, Michigan 48109-2140
2. Ford Motor Company, Dearborn, Michigan 48121
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1892
Reference12 articles.
1. Microstructural Design of Fiber Composites
2. Delamination Fracture Toughness of Woven-Fabric Composites Under Mixed-Mode Loading
3. Modified Mixed-Mode Bending Test Apparatus for Measuring Delamination Fracture Toughness of Laminated Composites
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