Equations of high frequency vibrations of thermopiezoelectric crystal plates
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...Suleman & Venkayya (1995a) and Suleman & Gonçalvès (1995) proposed a 4 node plate element using bilinear shape functions and the Mindlin assumption (constant shear angle) to accomodate thick as well as thin shells; each node has 5 degrees of freedom (3 translations and 2 rotations), the element has one additional electrical degree of freedom per piezoelectric layer (voltage across the thickness). It uses a reduced integration scheme for the transverse shear stiffness to avoid the transverse shear locking phenomenon. This element is demonstrated using the plate described by Crawley & Lazarus (1991), a bimorph pointer and panel flutter control; comparison with the work of Ha et al....
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...Suleman & Venkayya (1995a) and Suleman & Gonçalvès (1995) proposed a 4 node plate element using bilinear shape functions and the Mindlin assumption (constant shear angle) to accomodate thick as well as thin shells; each node has 5 degrees of freedom (3 translations and 2 rotations), the element has one additional electrical degree of freedom per piezoelectric layer (voltage across the thickness). It uses a reduced integration scheme for the transverse shear stiffness to avoid the transverse shear locking phenomenon. This element is demonstrated using the plate described by Crawley & Lazarus (1991), a bimorph pointer and panel flutter control; comparison with the work of Ha et al. (1992) is made....
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...Rao & Sunar (1993) established a finite element formulation of thermopiezoelectric problems starting from the linear thermopiezoelectric constitutive equations established by Mindlin (1974) and the Hamilton’s principle....
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...Rao & Sunar (1993) established a finite element formulation of thermopiezoelectric problems starting from the linear thermopiezoelectric constitutive equations established by Mindlin (1974) and the Hamilton’s principle. In (Sunar & Rao, 1996, 1997), they used the quasistatic equations of thermopiezoelectricity to develop heat, sensor and actuator equations; a finite element formulation is presented. A distributed control system consisting in a cantilever beam sandwiched between a piezoelectric sensor/actuator pair is used to evaluate the proposed finite element approach on the static and dynamic behaviour. Tzou & Ye (1996) derived a 12-nodes triangular thin solid plane element with 4 degrees of freedom per node; it uses shape functions quadratic in the two in-plane directions and linear in the transverse direction with the assumption of a layerwise constant shear angle (Mindlin hypothesis). A laminate is composed of laminae which could be either elastic material or piezoelectric material; the laminated structure is obtained by stacking elements together and connecting the corresponding nodes; this element is validated by modelling the actuation of a bimorph pointer. To stress the influence of the piezoelectric coupling on the vibration characteristics, a semicircular ring shell has been modelled using 60 triangular shell elements (20 for each layer and 10 element meshes along the length); the evolution of its eigenfrequencies with a growing number of short-circuited electrodes is examined. The number of short-circuited electrodes varies from 1 to 10 (fully short-circuited). This element has been extended later by Köppe et al. (1998) to isoparametric curved triangular and quadrangular elements with shape functions of different polynomial degree for each layer; the model is applied to a rectangular plate of composite material with surface bonded piezo patches under static voltage load, simply supported on two edges....
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...Suleman & Venkayya (1995a) and Suleman & Gonçalvès (1995) proposed a 4 node plate element using bilinear shape functions and the Mindlin assumption (constant shear angle) to accomodate thick as well as thin shells; each node has 5 degrees of freedom (3 translations and 2 rotations), the element has one additional electrical degree of freedom per piezoelectric layer (voltage across the thickness). It uses a reduced integration scheme for the transverse shear stiffness to avoid the transverse shear locking phenomenon. This element is demonstrated using the plate described by Crawley & Lazarus (1991), a bimorph pointer and panel flutter control; comparison with the work of Ha et al. (1992) is made. Chattopadhyay et al. (1999) developed a quasi-static coupled thermopiezoelectric model for a smart composite plate structure with surface bonded piezoelectric materials using a variational...
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