Buckling analysis of general composite laminates by hybrid-stress finite element method
Author:
Affiliation:
1. National Tsing Hua University, Hsinchu, Taiwan 30043, Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.10556
Reference17 articles.
1. ^oor, A. K. * 'Stability of Multilayered Composite Plates," Fibre Science Technology, Vol.8, 1975, pp.81-89.
2. Stability and vibration of isotropic, orthotropic and laminated plates according to a higher-order shear deformation theory
3. Stability and natural vibration analysis of laminated plates by using a mixed element based on a refined plate theory
4. A Simple Higher-Order Theory for Laminated Composite Plates
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3. Nonlinear buckling of fiber‐reinforced composite plates under hygrothermal effects;Journal of the Chinese Institute of Engineers;1996-09
4. Multilayer hybrid-stress finite element analysis of composite laminates with delamination cracks originating from transverse cracking;Engineering Fracture Mechanics;1996-07
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