Efficient higher order composite plate theory for general lamination configurations
Author:
Affiliation:
1. University of Washington, Seattle, Washington 98195
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference11 articles.
1. A High-Order Theory of Plate Deformation—Part 2: Laminated Plates
2. A Simple Higher-Order Theory for Laminated Composite Plates
3. Laminated Composite Plate Theory With Improved In-Plane Responses
4. Bending, vibration and buckling of simply supported thick multilayered orthotropic plates: An evaluation of a new displacement model
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