Interlaminar stress behavior of laminated composite plates under Low velocity Impact

저속충격을 받는 적층복합재료 평판의 미시구조를 고려한 interlaminar stress 거동 연구

  • 지국현 (서울대학교 기계항공공학부) ;
  • 김승조 (서울대학교 기계항공공학부, 비행체 특화연구센터)
  • Published : 2005.04.29

Abstract

Prediction of damage caused by low-velocity impact in laminated composite plate is an important problem faced by designers using composites. Not only the inplane stresses but also the interlaminar normal and shear stresses playa role in estimating the damage caused. The work reported here is an effort in getting better predictions of damage in composite plate using DNS approach. In the DNS model, we discretize the composite plates through separate modeling of fiber and matrix for the local microscopic analysis. Through comparison with the homogenized model. In the view of microscopic mechanics with DNS model, interlaminar stress behaviors in the inside of composite materials is investigated and compared with the results of the homogenized model which has been used in the conventional approach of impact analysis.

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