Dynamic analysis for delaminated composites using DKQ concept based on higher-order zig-zag theory

고차 지그재그 모델을 이용한 다중 층간 분리부가 내재한 복합재 평판의 동적 해석

  • 오진호 (서울대학교 기계항공공학부 대학원생) ;
  • 조맹효 (서울대학교 기계항공공학) ;
  • 김준식 (The Pennsylvania State University 항공우주공학과 대학원)
  • Published : 2002.10.01

Abstract

A higher-order zig-zag theory is developed to refine the predictions of natural frequency and mode shape of laminated composite plates with multiple delaminations. By imposing top and bottom surface transverse shear stress-free and interface continuity conditions of transverse shear stresses including delaminated interfaces, the displacement field with minimal degree-of-freedoms are obtained. This displacement field can systematically handle the number, shape, size, and locations of delaminations. Through the dynamic version of variational approach, the dynamic equilibriums and variationally consistent boundary conditions are obtained. Through the numerical example of natural frequency analysis, the accuracy and efficiency of present theory are demonstrated. The present theory is suitable as an efficient tool to analyze the static and dynamic behavior of the composite plates with multiple delaminations.

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