Nonlinear Vibrations of Circular Cylindrical Shells with Different Boundary Conditions
Author:
Affiliation:
1. Università di Parma, 43100 Parma, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2053
Reference26 articles.
1. Non-linear free vibration and postbuckling of symmetrically laminated orthotropic imperfect shallow cylindrical panels with two adjacent edges simply supported and the other edges clamped
2. Nonlinear vibration and postbuckling of unsymmetrically laminated imperfect shallow cylindrical panels with mixed boundary conditions resting on elastic foundation
3. Non-linear vibration and postbuckling of unsymmetric cross-ply circular cylindrical shells
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