Quenching Vibration on a Harmonically Excited Symmetric Laminated Composite Plate

Author:

Chen Jiawang1,Cha Philip D.2,Shen Yichang3,Zhou Xiang1

Affiliation:

1. Department of Aircraft Design, School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai 200240, China

2. Department of Engineering, Harvey Mudd College, Claremont, CA 91711

3. Institute of Mechanical Sciences and Industrial Applications, ENSTA Paris, Paris 91762, France

Abstract

Abstract In this paper, a simple and efficient method is developed to quench the steady-state vibration of a harmonically excited, damped and symmetric laminated composite rectangular plate. This is achieved by enforcing points of zero displacement, or nodes, at some specified locations on the laminated composite plate using properly tuned damped oscillators. Using the assumed-modes method, the governing equations of the laminated composite plate carrying the damped oscillators are first formulated. A set of constraint equations is established by enforcing nodes at user-specified locations on the plate. Two attachment scenarios are considered: when the attachment and node locations coincide and when they are distinct. Numerical experiments show that for both cases, the damped oscillator parameters can be readily determined and the desired node locations can be successfully imposed. More importantly, enforcing nodes can suppress vibration in the vicinity of the node locations, thereby keeping that region of the laminated composite plate nearly stationary.

Publisher

ASME International

Subject

General Engineering

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