Modeling a Piezothermoelastic Laminated Plate-Membrane
Source abstract
Abstract
Analysis of laminated piezopolymer actuated circular membranes is presented. The nonlinear equations of motion governing a continuous circular laminate of arbitrary thermal, electrical and mechanical properties are developed. Assuming axisymmetry, a closed-form asymptotic solution is developed using a combination of perturbation techniques. These governing equations are applied to a model laminate of Kapton and PVDF materials where static and dynamic results are discussed.
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Research context
OpenAlex topics: Aeroelasticity and Vibration Control · Composite Structure Analysis and Optimization · Structural Analysis and Optimization
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Affiliations
Air Force Research Laboratory, 2 Air Force Institute of Technology, WPAFB, OH 45433, USA,
Air Force Research Laboratory, 2Air Force Institute of Technology, WPAFB, OH 45433, USA
References (17)
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