Effect of interfacial imperfection on buckling and bending behavior of composite laminates
Author:
Affiliation:
1. University of Science and Technology of China, Hefei, Anhui 230026, People's Republic of China
2. University of Wales, Cardiff CF2 1XH, Wales, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.13443
Reference38 articles.
1. Assessment of Shear Deformation Theories for Multilayered Composite Plates
2. Theories and Computational Models for Composite Laminates
3. Bending, vibration and buckling of simply supported thick multilayered orthotropic plates: An evaluation of a new displacement model
4. An Improved Shear-Deformation Theory for Moderately Thick Multilayered Anisotropic Shells and Plates
5. Multilayered anisotropic plate models with continuous interlaminar stresses
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