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Article
Theory of Geometrically Nonlinear Composite Plates with Piezoelectric Stiffeners
American Society of Mechanical Engineers, Dynamic Systems and Control Division (Publication) DSC
  • Victor Birman, Missouri University of Science and Technology
Abstract

The governing equations for geometrically nonlinear, arbitrary laminated rectangular plates reinforced by the stiffeners that 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. 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.

Meeting Name
American Society of Mechanical Engineers, Dynamic Systems and Control Division (Publication) DSC (1992, Anaheim, CA, USA)
Department(s)
Mechanical and Aerospace Engineering
Document Type
Article - Conference proceedings
Document Version
Citation
File Type
text
Language(s)
English
Rights
© 1992 American Society of Mechanical Engineers (ASME), All rights reserved.
Publication Date
1-1-1992
Publication Date
01 Jan 1992
Citation Information
Victor Birman. "Theory of Geometrically Nonlinear Composite Plates with Piezoelectric Stiffeners" American Society of Mechanical Engineers, Dynamic Systems and Control Division (Publication) DSC (1992)
Available at: http://works.bepress.com/victor-birman/188/