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Article
Active Control of Composite Plates Using Piezoelectric Stiffeners
International Journal of Mechanical Sciences
  • Victor Birman, Missouri University of Science and Technology
Abstract

The governing equations for geometrically nonlinear, arbitrarily laminated rectangular plates reinforced by stiffeners which include piezoelectric and composite layers are presented. General equations obtained in the paper are reduced to a single equation of motion for piezoelectrically reinforced, geometrically linear, specially orthotropic plates. A criterion for an effective control of forced vibrations of such plates using piezoelectric stiffeners and a static electric field is illustrated. Active control of dynamic stability using a dynamic electric field with a frequency equal to that of the in-plane load is also considered. In addition, an approach to the analysis of piezoelectrically stiffened nonlinear plates whose motion is represented by single-term functions of the coordinates is discussed. Numerous active control problems can be addressed using the theory outlined in the paper. © 1993.

Department(s)
Mechanical and Aerospace Engineering
Document Type
Article - Journal
Document Version
Citation
File Type
text
Language(s)
English
Rights
© 1993 Elsevier, All rights reserved.
Publication Date
1-1-1993
Publication Date
01 Jan 1993
Citation Information
Victor Birman. "Active Control of Composite Plates Using Piezoelectric Stiffeners" International Journal of Mechanical Sciences (1993) ISSN: 0020-7403
Available at: http://works.bepress.com/victor-birman/1/