2016
DOI: 10.1016/j.sna.2016.01.054
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Modeling of plates with multiple anisotropic layers and residual stress

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Cited by 17 publications
(13 citation statements)
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“…The value of the tensile stress of the Si 3 N 4 is found by measuring the curvature of a double side polished wafer with a layer of Si 3 N 4 of known thickness on one side and then applying Stoney's equation. The tensile stress increases both the resonance frequency and pull-in voltage compared with a similar plate with no stress [11].…”
Section: Devicesmentioning
confidence: 94%
“…The value of the tensile stress of the Si 3 N 4 is found by measuring the curvature of a double side polished wafer with a layer of Si 3 N 4 of known thickness on one side and then applying Stoney's equation. The tensile stress increases both the resonance frequency and pull-in voltage compared with a similar plate with no stress [11].…”
Section: Devicesmentioning
confidence: 94%
“…(15) and approximates the first mode-shape of the circular plate. Moreover, it has been employed in electrostatic analysis of circular microplate, previously [4,24].…”
Section: Differential Equation For the One-sided Cmutmentioning
confidence: 99%
“…For all of these studies mentioned above, methodology of analysis comprise either lumped element models (LEM) [3,17] or continuum models, such as plate [2,12] or membrane models [22,23]. Membrane models have a low accuracy because the flexural rigidity of the microplate is negligible [24]. LEM is a simple method that has been frequently utilized for modeling of both one-sided and two-sided CMUTs, but it lacks sufficient level of accuracy for describing the static pull-in voltage and dynamics of the system, particularly in higher frequencies [5,17].…”
Section: Introductionmentioning
confidence: 99%
“…Because the integration is performed over the entire region, the modal contours of the DFUT for CMUT operation can be plotted. At the fundamental thickness-bending vibration mode, the relative deflection of the laminated plates is given to be [ 24 , 33 , 34 ]: where W 0 is the center deflection, α is the plate shape factor, related to the geometric parameters of the DFUT and the orientation of the anisotropic materials.…”
Section: Theoretical Analysis and Modellingmentioning
confidence: 99%