Finite element for composite plate bending based on efficient higher order theory
Author:
Affiliation:
1. University of Washington, Seattle, Washington 98195
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.12283
Reference24 articles.
1. Analysis of laminated composite plates using a higher-order shear deformation theory
2. A refined mixed shear flexible finite element for the nonlinear analysis of laminated plates
3. Buckling and vibration of laminated composite plates using various plate theories
4. A simple finite element formulation of a higher-order theory for unsymmetrically laminated composite plates
5. A Simple Higher-Order Theory for Laminated Composite Plates
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