Zigzag theory for composite laminates
Author:
Affiliation:
1. Michigan State University, East Lansing, Michigan 48824
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference8 articles.
1. Discussion: “Timoshenko Beam Theory Is Not Always More Accurate Than Elementary Beam Theory” (Nicholson, J. W., and Simmonds, J. G., 1977, ASME J. Appl. Mech., 44, pp. 337–338)
2. An Interlaminar Shear Stress Continuity Theory for Both Thin and Thick Composite Laminates
3. Development of an anisotropic, multilayered, shear-deformable rectangular plate element
4. Laminated Composite Plate Theory With Improved In-Plane Responses
5. An improved zig-zag model for the bending of laminated composite plates
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