Abstract
After the Hamilton principle for thermo-mechanical-electric coupling problem is derived, the third-order shear deformation theory is extended to encompass piezothermoelastic laminated plates. Based on the velocity feedback control, a model for the active vibration control of laminated plates with piezothermoelastic sensor/actuator is established. An analytical solution is obtained for the case of general forces acting on a simply supported piezothermoelastic laminated plate. Numerical results are presented. The factors that influence the controlled responses of the plate are examined.
| Original language | English |
|---|---|
| Pages (from-to) | 1925-1947 |
| Number of pages | 23 |
| Journal | International Journal of Solids and Structures |
| Volume | 36 |
| Issue number | 13 |
| DOIs | |
| State | Published - 1 May 1999 |
| Externally published | Yes |
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