Curved piezoactuator model for active vibration control of cylindrical shells-Reference-Cited by-同舟云学术

Curved piezoactuator model for active vibration control of cylindrical shells

Published:1996-05 Issue:5 Volume:34 Page:1034-1040
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Sonti Venkata R.¹,Jones James D.²

Affiliation:

1. Automated Analysis Corporation, Peoria, Illinois 61602

2. Purdue University, West Lafayette, Indiana 47907-1077

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.13184

Reference18 articles.

1. Distributed piezoelectric-polymer active vibration control of a cantilever beam

2. Piezoelectric Actuators for Distributed Vibration Excitation of Thin Plates

3. 4Lee, C. K. "Piezoelectric Laminates for Torsional and Bending Modal Control: Theory and Experiment," Ph.D. Thesis,Dept. of Mechanical Engineering, Cornell Univ., Ithaca, NY,May 1987.

4. Active control of interior noise in model aircraft fuselages using piezoceramic actuators

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