Understanding the fatigue behavior of carbon fiber reinforced plastics (CFRP) requires clarifying the mechanism of interfacial crack initiation and propagation along individual carbon fibers. In this study, in-situ synchrotron radiation X-ray nano-computed tomography (nano-CT) was employed to visualize three-dimensional interfacial crack propagation between a single carbon fiber and an epoxy matrix under cyclic loading. Dumbbell-shaped specimens containing a transversely embedded carbon fiber were subjected to cyclic loading at maximum stresses of 50 and 60 MPa, both below the yield stress (70 MPa). Crack propagation was captured after specific numbers of cycles using a custom-designed piezo-actuated fatigue testing system installed at beamline BL20XU of the SPring-8 synchrotron facility. The reconstructed nano-CT images revealed that interfacial cracks initiated from the fiber ends and propagated several micrometers along the interface. The measured crack propagation rate decreased with increasing cycle number and eventually indicated a transition to non-propagating cracks. The corresponding stress intensity factor range calculated at the crack tips was lower than the experimentally determined threshold value for the bulk epoxy matrix obtained using compact tension specimens. This comparison confirms that the interfacial crack along a single carbon fiber is too small to fracture the surrounding epoxy matrix, suggesting that fatigue behavior is governed by the local fracture toughness of the epoxy matrix. These findings demonstrate, for the first time, direct three-dimensional visualization of an interfacial crack along a single carbon fiber under elastic cyclic loading, providing new insights into the micro-mechanical origins of fatigue resistance in CFRP materials.
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