2004
DOI: 10.1016/j.ijsolstr.2004.02.058
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A finite element model for the static and dynamic analysis of a piezoelectric bimorph

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Cited by 148 publications
(103 citation statements)
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“…These theories yield excellent accuracy, but the computational effort increases in proportion to the number of layers, which restricts their application for practical dynamics and control problems. Mixed coupled equivalent single layer (ESL) theories such as the first-order shear deformation theory (FSDT) [Saravanos 1999;Wang 2004] and refined third-order theory (TOT) [Correia et al 2000], considering a global variation for the displacements across the entire thickness and a layerwise distribution for the electric potential, have been employed for the dynamic analysis of hybrid plates. It is now well known that since these theories do not account for the layerwise (zigzag) nature of distributions of the inplane displacements, they yield inaccurate results for moderately thick laminates and even thin laminates with strong inhomogeneity across the thickness.…”
Section: Introductionmentioning
confidence: 99%
“…These theories yield excellent accuracy, but the computational effort increases in proportion to the number of layers, which restricts their application for practical dynamics and control problems. Mixed coupled equivalent single layer (ESL) theories such as the first-order shear deformation theory (FSDT) [Saravanos 1999;Wang 2004] and refined third-order theory (TOT) [Correia et al 2000], considering a global variation for the displacements across the entire thickness and a layerwise distribution for the electric potential, have been employed for the dynamic analysis of hybrid plates. It is now well known that since these theories do not account for the layerwise (zigzag) nature of distributions of the inplane displacements, they yield inaccurate results for moderately thick laminates and even thin laminates with strong inhomogeneity across the thickness.…”
Section: Introductionmentioning
confidence: 99%
“…Boundaries are considered to be simply supported. Also, its material constants are [24]: c = In Figure 2, the through-the-thickness variation of de ection, W , at the plate center is shown and the results are compared with those of Wang [24]. From this gure, it is clear that in the present analysis, modeling of the piezoelectric material is done properly.…”
Section: Piezoelectric Bimorph Actuator Platementioning
confidence: 87%
“…, where indices α denotes multiplication without summation (vectorisation) 3 Solution at the time t + ∆t using vectorisation u α t+∆t =M αRα 3 u t−∆t = u t , u t = u t+∆t , t = t + ∆t approaches given in [11]. The error was less than 2% for maximum deflection (L/h = 10) and 0% for electric potential in comparison to full 3D finite element modell (ANSYS SOLID5 9600 elements).…”
Section: Solving Equation Of Motionmentioning
confidence: 99%
“…The second problem is actuation and reception of elastic waves in aluminium plate of dimensions 315x315x1 mm 3 by circular and rectangular PZT-4 piezoelectric ceramics perfectly bonded to the surface of the plate. Piezoelectric material constants can be found in [11], whereas for aluminium it has been assumed: Young modulus E = 71GP a, Poisson ratio 0.33, mass density ρ = 2700 kg/m 3 . It has been assumed that excitation signal is five tone burst sine modulated by Hanning window with the carrier frequency of 100 kHz.…”
Section: Solving Equation Of Motionmentioning
confidence: 99%
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