导航

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2007, Vol. 28 ›› Issue (1): 100-105.

Previous Articles     Next Articles

Non-Stationary Random Vibration Analysis of Composite Laminated Structures Attached with Frequency-Dependant Damping Layer

DAI Xin-jin,LIN Jia-hao,CHEN Hao-ran   

  1. State Key Laboratory of Structural Analysis for Industrial Equipment , Dalian University of Technology 
  • Received:2005-08-30 Revised:2006-06-22 Online:2007-01-10 Published:2007-01-10
  • Contact: LIN Jia-hao

Abstract:

An efficient and accurate non-stationary random vibration algorithm for the composite laminated structures attached with viscoelastic damping layer is proposed. Both the Adams damping of the composite laminated structures and the attached frequency-dependant damping are taken into account in the analysis. For the resulting non-classically damped and frequency-dependant complex system, in combination with the real-mode-based degree-reduction scheme, the pseudo excitation method is developed and the precise integration method is applied to solve the reduced non-stationary random vibration equation.

Key words: composite,  , pseudo , excitation , method, precise , integration , method , non-stationary , random , vibra-tion, frequency-dependant , damping

CLC Number: