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Fatigue damage detection of CFRP using the electrical resistance change method
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  • Fatigue damage detection of CFRP using the electrical resistance change method
  • Fatigue damage detection of CFRP using the electrical resistance change method
저자명
Todoroki. Akira,Mizutani. Yoshihiro,Suzuki. Yoshiro,Haruyama. Daichi
간행물명
International journal of aeronautical and space sciences
권/호정보
2013년|14권 4호|pp.350-355 (6 pages)
발행정보
한국항공우주학회
파일정보
정기간행물|ENG|
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이 논문은 한국과학기술정보연구원과 논문 연계를 통해 무료로 제공되는 원문입니다.
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기타언어초록

Electrical resistance change measurements were performed, to detect fatigue damage of a quasi-isotropic CFRP and cross-ply CFRP laminates. A four-probe method was used to measure the exact electrical resistance change. A three-probe method was used to measure the electrical contact resistance change, during long cyclic loading. The specimen side surface was observed using a video-microscope to detect damage. The measured electrical resistance changes were compared with the observed damage. The results of this study show that the electrical resistance increase of the quasi-isotropic laminate was caused by a delamination crack between ${pm}45^{circ}$ plies. Matrix cracking caused a small electrical resistance increase of the cross-ply laminate, but the decreased electrical resistance caused by the shear-plastic deformation impedes matrix-cracking detection.