2002
DOI: 10.1299/jsmec.45.8
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Micro-Control Actions of Segmented Actuator Patches Laminated on Deep Paraboloidal Shells.

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Cited by 28 publications
(5 citation statements)
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“…Although the parabolic cylindrical shell panels generally vibrate in three directions, that is, u i ( i = x , ψ , 3 ) , the transverse vibration u 3 ( x , ψ , t ) usually is the dominant dynamic response of the shell structure, and the longitudinal and meridional vibrations are often small and negligible (Tzou, 2018; Tzou et al, 2002). Thus, in the following analysis, only the transverse vibration is considered.…”
Section: Parabolic Cylindrical Shell Model and Dynamic Equationsmentioning
confidence: 99%
“…Although the parabolic cylindrical shell panels generally vibrate in three directions, that is, u i ( i = x , ψ , 3 ) , the transverse vibration u 3 ( x , ψ , t ) usually is the dominant dynamic response of the shell structure, and the longitudinal and meridional vibrations are often small and negligible (Tzou, 2018; Tzou et al, 2002). Thus, in the following analysis, only the transverse vibration is considered.…”
Section: Parabolic Cylindrical Shell Model and Dynamic Equationsmentioning
confidence: 99%
“…xsin(β * )dψdx. (10) The electric control forces and moments induced by the actuator per unit length with control voltage φ a are defined as [13] N…”
Section: Formulations Of the Modal Control Forcementioning
confidence: 99%
“…Examples include aerospace/aircraft structures [27,28], robot manipulators [29], vibration controls and isolations, high-precision devices, microsensors/actuators, thin-film MEMS [30], health monitoring [31], microdisplacement actuation and control [25], and so on. Additional applications in smart structures and structronic systems encompass distributed structural control [16,[32][33][34][35][36], rotor dynamics control [37], self-sensing actuators [38][39][40], orthogonal modal sensors/actuators [41][42][43], space truss members [44], noise control [45], vibration isolators [46], active constrained damping [47], morphing of wings and blades [48], microscopic neural-sensing and actuation characteristics of conical, paraboloidal, toroidal and spherical structronic shells [49][50][51][52][53][54][55], and so on. Other recent practical applications include piezoelectrically damped skis, control of aeroelastic wing flutter, optical metering truss control, helicopter blade control, noise reduction, biomedical applications, and ultrasonic motors [56][57][58][59][60][61].…”
Section: Piezoelectric Materialsmentioning
confidence: 99%