Akira Todoroki, Yoshihiro Mizutani, Yoshiro Suzuki and Daichi Haruyama
International Journal of Aeronautical and Space Sicences, vol. 14, no. 4, pp.350-355, 2013

Abstract : 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 ±45° 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.

Keyword : Composites, Electrical resistance, Carbon Fibers, Delamination