Exact Solutions of Cross-Ply Laminates with Bonding Imperfections
Author:
Affiliation:
1. Zhejiang University, 310027 Hangzhou, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.6817
Reference27 articles.
1. Thermoelastic analysis of layered structures with imperfect layer contact
2. Buckling and postbuckling behavior of delaminated sandwich beams
3. Effect of interfacial imperfection on buckling and bending behavior of composite laminates
4. Theory for Multilayered Anisotropic Plates With Weakened Interfaces
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