This paper presents modal sensitivity factors, actuation factors and controlled damping ratio for segmented distributed piezoelectric sensor and actuator layers laminated on simply supported thick rectangular plates and circular cylindrical shells made of cross-ply composite laminate. A Flugge-type
SEGMENTED SENSORS AND ACTUATORS FOR THICK PLATES AND SHELLS PART II: PARAMETRIC STUDY
โ Scribed by P.C. DUMIR; G.P. DUBE; C. BALAJI KUMAR
- Publisher
- Elsevier Science
- Year
- 1999
- Tongue
- English
- Weight
- 165 KB
- Volume
- 226
- Category
- Article
- ISSN
- 0022-460X
No coin nor oath required. For personal study only.
โฆ Synopsis
A parametric study is presented here for the modal sensitivity and actuation factors and controlled damping ratio for the rectangularly segmented distributed piezoelectric sensor and actuator layers laminated on simply supported thick rectangular plates and circular cylindrical shells made of cross ply composite laminate. The analytical expressions of these entities, developed in Part I of this two-part study, based on a Flugge-type "rst order shear deformation theory (FSDT) and classical lamination theory (CLT), are numerically evaluated to illustrate the e!ect of the thickness parameter. The contribution of the membrane and bending strains to sensitivity and actuation factors is computed for plates and shells for the lowest mode and a few higher modes. It has been concluded that the classical lamination theory is inadequate for the analysis of spatial actuation and control of all modes for thick plates and shells as well as for the higher modes of thin composite plates and shells.
๐ SIMILAR VOLUMES
Distributed piezoelectric layers can be used as distributed sensors and actuators for structural monitoring and control of elastic continua. In this paper, distributed vibration sensing and control of continua using single-piece symmetrically distributed and multi-piece segmented sensors/actuators a
It was noted that a fully (symmetrically) distributed piezoelectric sensor/actuator could lead to minimum, or zero, sensing/control effects for antisymmetrical modes of structures, especially with symmetrical boundary conditions. One method to improve the performance is to segment the symmetrically