NASA NTRS · 19960047606
Layerwise Finite Elements for Smart Piezoceramic Composite Plates in Thermal Environments
Abstract
Analytical formulations are presented which account for the coupled mechanical, electrical, and thermal response of piezoelectric composite laminates and plate structures. A layerwise theory is formulated with the inherent capability to explicitly model the active and sensory response of piezoelectric composite plates having arbitrary laminate configurations in thermal environments. Finite element equations are derived and implemented for a bilinear 4-noded plate element. Application cases demonstrate the capability to manage thermally induced bending and twisting deformations in symmetric and antisymmetric composite plates with piezoelectric actuators, and show the corresponding electrical response of distributed piezoelectric sensors. Finally, the resultant stresses in the thermal piezoelectric composite laminates are investigated.
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Saravanos, Dimitris A., Lee, Ho-Jun. 1996-07-01. Layerwise Finite Elements for Smart Piezoceramic Composite Plates in Thermal Environments. https://ntrs.nasa.gov/citations/19960047606
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