Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
510768 | Computers & Structures | 2006 | 8 Pages |
Abstract
Elasticity solution is presented for infinitely long, simply-supported, orthotropic, piezoelectric shell panel under dynamic pressure excitation. The direct and inverse piezoelectric effects are considered. The highly coupled partial differential equations (p.d.e.) are reduced to ordinary differential equations (o.d.e.) with variable coefficients by means of trigonometric function expansion in circumferential direction. The resulting ordinary differential equations are solved by the finite element method. Numerical examples are presented for [0/90/P] lamination, where P indicates the piezoelectric layer. Finally the results are compared with the published results.
Related Topics
Physical Sciences and Engineering
Computer Science
Computer Science Applications
Authors
M. Shakeri, M.R. Eslami, A. Daneshmehr,