Strength of Composite Laminates Containing Holes and Subjected to Complex Loading Conditions
Author:
Affiliation:
1. Saab Military Aircraft, S-58188 Linkoping, Sweden
2. Department of Lightweight Structures, The Royal Institute of Technology, S-10044 Stockholm, Sweden
Abstract
Publisher
SAGE Publications
Subject
Materials Chemistry,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites
Link
http://journals.sagepub.com/doi/pdf/10.1177/002199839703101203
Reference18 articles.
1. Behavior of graphite/epoxy plates with holes under biaxial loading
2. Biaxial testing of [O2/±45] s graphite/epoxy plates with holes
3. Mixed-mode fracture of notched composite laminates under uniaxial and multiaxial loading
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