Dynamic Responses of Smart Composites Using a Coupled Thermo-Piezoelectric-Mechanical Model
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/10.2514/2.848
Reference11 articles.
1. Use of piezoelectric actuators as elements of intelligent structures
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4. New higher order plate theory in modeling delamination buckling of composite laminates
5. Equations of high frequency vibrations of thermopiezoelectric crystal plates
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