Abstract
Extensive microstructural evaluations were performed on two titanium matrix composite (TMC) materials to examine any chemical and/or physical differences which explain fatigue crack growth patterns observed in these materials. These examinations included optical microscopy, scanning electron microscopy (SEM), energy dispersive X-ray (EDX) and Auger analysis. The results of these studies indicate that fatigue damage modes, in addition to being affected by obvious parameters like load and temperature are also affected by the process in which the TMC is consolidated. Fiber surface damage is visible on one of the two TMC systems which may have influenced the observed fatigue damage mode. The fiber surface damage can be traced back to the pressure applied to the laminate during consolidation. This paper provides a detailed explanation for the occurrence of the different fatigue damage modes and, therefore, provides an explanation for the significant difference in fatigue life of the two materials.
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