Effects of large deflection and transverse shear on response of rectangular symmetric composite laminates subjected to acoustic excitation
Author:
Affiliation:
1. Old Dominion University, Norfolk, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1987-933
Reference42 articles.
1. On Large Deflection Analysis in Acoustic Fatigue Design
2. Nonlinear multimode response of clamped rectangular plates to acoustic loading
3. Large deflection, large amplitude vibrations and random response of symmetrically laminated plates
4. Response of geometrically nonlinear elastic structures to acoustic excitation—an engineering oriented computational procedure
5. Large-Amplitude Random Response of Angle-Ply Laminated Composite Plates
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