Coupled Thermo-Piezoelectric-Mechanical Model for Smart Composite Laminates
Author:
Affiliation:
1. Arizona State University, Tempe, Arizona 85287-6106
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.645
Reference16 articles.
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4. Electromechanics and Vibrations of Piezoelectric Shell Distributed Systems
5. Dynamic modeling of piezoelectric laminated plates using finite element method
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