Consistent Methodology for the Modeling of Piezolaminated Shells
Author:
Affiliation:
1. Technion-Israel Institute of Technology, Haifa 32000, Israel
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.263
Reference17 articles.
1. Use of piezoelectric actuators as elements of intelligent structures
2. The Pin-Force Model Revisited
3. Pin-force and Euler-Bernoulli models for analysis of intelligent structures
4. Piezoelectric Actuators for Distributed Vibration Excitation of Thin Plates
5. Laminate Plate Theory for Spatially Distributed Induced Strain Actuators
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