Özet
An analytical model is presented to predict the nonlinear response of a double-wall sandwich cylindrical shell system subjected to random excitation. Nonlinear spring-dashpot models are integrated into the system to characterize the behavior of the soft core. Donnell's thin shell theory is used to develop the governing nonlinear equations of motion. A Monte Carlo simulation of stationary random processes, multimode Galerkin-type approach, and numerical integration procedures are used to develop linear and nonlinear response solutions of simply supported cylindrical shells. Numerical results include time domain response histories, root-mean-square values and response spectral densities. Parametric studies are performed to investigate the effects of nonlinearity, shell thickness, core stiffness, and thickness.
| Orijinal dil | İngilizce |
|---|---|
| Sayfa (başlangıç-bitiş) | 46-54 |
| Sayfa sayısı | 9 |
| Dergi | Journal of Aerospace Engineering |
| Hacim | 19 |
| Basın numarası | 1 |
| DOI'lar | |
| Yayın durumu | Yayınlandı - 2006 |
Parmak izi
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