The Effect of Transverse Shear on the Optimal Design of a Composite Plate
Author:
Affiliation:
1. The Boeing Company
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-9237
Reference4 articles.
1. On the Choice of Shear Correction Factor in Sandwich Structures
2. Mechanics of Laminated Composite Plates and Shells
3. 4N. Rastogi. Buckling of LaminatedComposite Plates Subject to Combined In-Plane Bi-Axial And Shear Loads. AIAA 2009-2453
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