Efficient Higher-Order Shell Theory for Laminated Composites with Multiple Delaminations
Author:
Affiliation:
1. Inha University, Inchon 402-751, Republic of Korea
2. Seoul National University, Seoul 151-742, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2031
Reference21 articles.
1. Assessment of Computational Models for Multilayered Composite Shells
2. Theories and Computational Models for Composite Laminates
3. A Refined Theory for Laminated Anisotropic, Cylindrical Shells
4. A higher-order shear deformation theory of laminated elastic shells
5. General two-dimensional theory of laminated cylindrical shells
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