| contributor author | Vedat Dogan | |
| contributor author | Rimas Vaicaitis | |
| date accessioned | 2017-05-08T21:16:15Z | |
| date available | 2017-05-08T21:16:15Z | |
| date copyright | January 2006 | |
| date issued | 2006 | |
| identifier other | %28asce%290893-1321%282006%2919%3A1%2846%29.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/45049 | |
| description abstract | 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. | |
| publisher | American Society of Civil Engineers | |
| title | Nonlinear Response of Double-Wall Cylindrical Shell Vibrations under Random Excitation | |
| type | Journal Paper | |
| journal volume | 19 | |
| journal issue | 1 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)0893-1321(2006)19:1(46) | |
| tree | Journal of Aerospace Engineering:;2006:;Volume ( 019 ):;issue: 001 | |
| contenttype | Fulltext | |