Free Vibration of Thick Quadrilateral Laminates Using Third-Order Shear-Normal Deformation Theory
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24060
Funder
Virginia Tech
ONR
Office of Naval Research
State University
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference54 articles.
1. XVI. The small free vibrations and deformation of a thin elastic shell
2. On transverse bending of plates, including the effect of transverse shear deformation
3. Recent advances in analysis of laminated beams and plates. Part I - Sheareffects and buckling.
4. PLANE WAVE SOLUTIONS AND MODAL ANALYSIS IN HIGHER ORDER SHEAR AND NORMAL DEFORMABLE PLATE THEORIES
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