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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2007, Vol. 28 ›› Issue (增): 109-115.

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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:2006-10-25 Revised:2006-12-25 Online:2007-08-10 Published:2007-08-10
  • Contact: LIN Jiahao

Abstract:

An efficient and accurate non-stationary random vibration algorithm for the composite laminated structures attached with viscoelastic damping layer was proposed. Both the Adams damping of the composite laminated structures and the attached frequencydependant damping were 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 was developed and the precise integration method was applied to solve the reduced non-stationary random vibration equation.

Key words: composite,  , frequencydependant , damping,  , pseudo , excitation , method,  , random , vibration

CLC Number: