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A Finite Element Adaptive Plate Model

  • A. Suleman
Part of the International Centre for Mechanical Sciences book series (CISM, volume 429)

Abstract

A simple quadrilateral shell finite element has been formulated for the analysis of adaptive laminated composite plates. The finite element is quadrilateral in shape and has 4 nodal points with 24 degrees of freedom.

Keywords

Coefficient Ofthermal Expansion Piezoelectric Actuator Piezoelectric Layer Piezoelectric Bimorph Geometric Stiffness Matrix 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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References

  1. 1.
    I. Suleman and V.B. Venkayya, “A Simple Finite Element Foramlation for a Laminated Composite Plate with Piezoelectric Layers”, Journal of Intelligent Materials Systems and Stnm coures,Vol. 6, No. 6, pp. 776–782, Nov. 95.CrossRefGoogle Scholar
  2. 2.
    II.S. Tzou, and C.I. Tseng, “Distributed Piezoelectric Sensor/Actuator Design for 4,- namic Measurement/Control of Distributed Parameter Systems: a Piezoelectric Finite Element Approach”, Journal of Sound and Vibration, Vol. 138, No. 1, 1990, pp. 17–34.CrossRefGoogle Scholar
  3. 3.
    E.F. Crawley, and K.B. Lazarus, ‘Induced Strain Actuation of isotropic and Anisotropie Plates“, AIAA Journal, Vol. 29, No. 6, 1991, pp. 944–951.CrossRefGoogle Scholar

Copyright information

© Springer-Verlag Wien 2001

Authors and Affiliations

  • A. Suleman
    • 1
  1. 1.IDMEGInstituto Superior TécnicoLisbonPortugal

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