Dynamic model updating of the laminated composite plate using natural frequencies measured from modal test

고유진동수의 실험값을 사용한 복합재 적층판의 동적 모델링 개선

  • 홍단비 (서울대학교 대학원 항공우주공학과) ;
  • 유정규 (국방과학연구소) ;
  • 박성호 (서울대학교 대학원 항공우주공학과) ;
  • 김승조 (서울대학교 공과대학 항공우주공학과)
  • Published : 1998.04.01

Abstract

In order to improve the prediction of dynamic behavior in structures, several lower vibration modes from FFT analysis through experiments are used to update the mechanical properties followed by the updated frequencies from numerical analysis. Performance index consists of the sum of error norms between the chosen frequencies and corresponding frequencies from numerical analysis. As an updating process of the natural frequencies, the optimization algorithm based on conjugate gradient method is adopted. The gradient of performance index is calculated using the sensitivity of selected eigenvalues with respect to each design parameter. The mechanical properties of lamina, E$\_$l/, E$\_$2/, .nu.$\_$12/ and G$\_$12/, are design parameters for the updating process. The proposed method is applied to predict the dynamic behavior of composite laminated plates of [0]$\_$8T/ and [.+-.45]$\_$2S/ separately or interchangeably. Also, the mixed case for [0]$\_$8T/ and [.+-.45]$\_$2S/ is exarm'ned to check the possibility for the improved prediction generally. The good agreement is obtained between the measured frequencies and the numerical ones. Based on the results for all the cases studied, the proposed approach has a clear potential in characterizing the mechanical properties of composite lamina.

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