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학술논문한국기계항공기술학회지2017.02 발행KCI 피인용 8

유한요소 해석법을 이용한 단방향 CFRP에서의 중앙크랙 진전에 의한 파괴 거동 연구

A Study of Fracture Behavior due to the Propagation of Center Crack at Unidirectional CFRP through Finite Element Analysis

박재웅(공주대학교); 조재웅(공주대학교)

19권 1호, 21~26쪽

초록

At modern mechanical and automotive industry, the material with light weight proceeds in order to thr environmental issue and high performance. Machine part is fastened with numbers of bolts and nuts. Generally, the metal part at mechanical structure is fastened with bolt and nut through puncturing. But it is difficult to puncture at CFRP with the property of fiber structure like the general metal. In this study, the fracture behavior is investigated by the hole and crack at the plate of the unidirectional CFRP due to ply angle. The thickness of plate is 2 mm. Two laminates with the varied ply angles are layered and eight plies are made. The hole is placed at the center of plate and the cracks with the length of 2 mm are generated on both left and right sides from the hole. The finite element program of ANSYS is carried out in order to analyze the CFRP with fiber layer. As analysis, the maximum reaction force and equivalent stress are investigated due the angle of ply. The reaction force in case of the stacking angle of 90° is shown to be greatest among all specimens.

Abstract

At modern mechanical and automotive industry, the material with light weight proceeds in order to thr environmental issue and high performance. Machine part is fastened with numbers of bolts and nuts. Generally, the metal part at mechanical structure is fastened with bolt and nut through puncturing. But it is difficult to puncture at CFRP with the property of fiber structure like the general metal. In this study, the fracture behavior is investigated by the hole and crack at the plate of the unidirectional CFRP due to ply angle. The thickness of plate is 2 mm. Two laminates with the varied ply angles are layered and eight plies are made. The hole is placed at the center of plate and the cracks with the length of 2 mm are generated on both left and right sides from the hole. The finite element program of ANSYS is carried out in order to analyze the CFRP with fiber layer. As analysis, the maximum reaction force and equivalent stress are investigated due the angle of ply. The reaction force in case of the stacking angle of 90° is shown to be greatest among all specimens.

발행기관:
한국기계항공기술학회
DOI:
http://dx.doi.org/10.17958/ksmt.19.1.201702.21
분류:
기계공학

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유한요소 해석법을 이용한 단방향 CFRP에서의 중앙크랙 진전에 의한 파괴 거동 연구 | 한국기계항공기술학회지 2017 | AskLaw | 애스크로 AI