Nonlinear response of double-wall cylindrical shell vibrations under random excitation

Dogan V. Z. , VAICAITIS R.

JOURNAL OF AEROSPACE ENGINEERING, vol.19, no.1, pp.46-54, 2006 (Peer-Reviewed Journal) identifier identifier

  • Publication Type: Article / Article
  • Volume: 19 Issue: 1
  • Publication Date: 2006
  • Doi Number: 10.1061/(asce)0893-1321(2006)19:1(46)
  • Journal Indexes: Science Citation Index Expanded, Scopus
  • Page Numbers: pp.46-54


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.