Vibration of a laminated composite plate is controlled by passive and active control methods. Stiffness change in composite structures by changes in laminate orientation is used as an example of a passive control method, negative velocity feedback control with the piezoelectric sensor/actuator is us
DAMPED VIBRATION OF COMPOSITE PLATES WITH PASSIVE PIEZOELECTRIC-RESISTOR ELEMENTS
โ Scribed by D.A. Saravanos
- Publisher
- Elsevier Science
- Year
- 1999
- Tongue
- English
- Weight
- 262 KB
- Volume
- 221
- Category
- Article
- ISSN
- 0022-460X
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โฆ Synopsis
Mechanics for the analysis of damping in composite plates with multiple resistively shunted piezoelectric layers are developed. The mixed ยฎeld piezoelectric laminate theory is extended to include distributed passive electric circuitry embedded or attached to piezoelectric layers. The equations of motion for the coupled laminate/circuitry system are formulated and exactly solved for the case of simply-supported plates. The modal frequencies and damping are directly calculated from the complex eigenvalues of the damped plate. The forced vibration of the damped piezoelectric composite plate is also directly predicted. Numerical results for a cross-ply graphite/epoxy plate with surface mounted resistively shunted piezoceramic layers are presented. The results show that for each mode there is an optimal resistance value which adds signiยฎcant modal damping. Away from this optimal value the modal damping gradually reduces to zero. Simultaneous shifting of the corresponding modal frequency to a higher value occurs over this optimal resistance range. The calculated frequency response of the damped plate illustrates that substantial vibration control of select modes can be obtained by proper tuning of the shunting resistive circuit.
๐ SIMILAR VOLUMES
A finite element formulation is presented to model the dynamic as well as static response of laminated composite plates containing integrated piezoelectric sensors and actuators subjected to both mechanical and electrical loadings. The formulation is based on the classical laminated plate theory and
A finite element model based on third order laminate theory is developed for the active position control and vibration control of composite beams with distributed peizoelectric sensors and actuators. The direct peizoelectric equation is used to calculate the total charge created by the strains on th