2002
DOI: 10.1177/104538902761696760
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FE Analysis of Piezo-Laminate Composites Under Thermal Loads

Abstract: A shear flexible 4-noded finite element formulation, having five mechanical degrees of freedom per node, is presented for modeling the dynamic as well as the static thermal response of laminated composites containing distributed piezoelectric layers. This element has been developed to have one electrical degree of freedom per piezoelectric layer. The mass, stiffness and thermo-electro-mechanical coupling effects on the actuator and sensor layers have been considered. Numerical studies have been conducted to in… Show more

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Cited by 11 publications
(7 citation statements)
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“…Our approach is clearly associated with the last item and in this field, we can point out a first family of electric potential approximations, see Suleman and Venkayya [10], Correia et al [7], Bansal and Ramaswamy [11], Mukherjee and Joshi [12], using only one dof for each piezoelectric lamina. Unfortunately, this layerwise approximation is not efficient for all situations as it will be seen later.…”
Section: Introductionmentioning
confidence: 99%
“…Our approach is clearly associated with the last item and in this field, we can point out a first family of electric potential approximations, see Suleman and Venkayya [10], Correia et al [7], Bansal and Ramaswamy [11], Mukherjee and Joshi [12], using only one dof for each piezoelectric lamina. Unfortunately, this layerwise approximation is not efficient for all situations as it will be seen later.…”
Section: Introductionmentioning
confidence: 99%
“…Example 1. In this example a plate with dimensions of 25.4 mm 3 × 25.4 mm 3 × 1.27 mm 3 and with the layers of [0/90/±45/p] s composed of carbon/graphite with attached piezoceramic layer under temperature gradient is investigated and the results compared with the data reported by Bansal et al [23] (Fig. 2).…”
Section: Numerical Results and Discussion 41 Comparison Studymentioning
confidence: 62%
“…In the previous section, the finite element approximations for the mechanical part were defined and elementary stiffness ½K e uu and mass ½M e uu matrices can be deduced from respectively Eqs. (10) and (11). They have the following expressions:…”
Section: The Elementary Matricesmentioning
confidence: 99%