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Direct observation on fatigue crack growth behavior in SiC (SCS-6) fiber-reinforced Ti-15-3 alloy matrix composite subjected to a constant tension-tension loading mode was performed by scanning electron microscope using a single edge-notched specimen in vacuum at room temperature and 550 o C. The fatigue crack growth rate at 550 o C was lower than that at room temperature, and the...
The debonding mechanism of an interphase in layered and fiber-reinforced composites was investigated with an emphasis on crack deflection and penetration. A single-edged notched model consisting of three phases was analyzed by the boundary element method. The dependence of elastic fields involved in the model on elastic constant combinations was revealed. Interfacial debonding other than the competition...
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