Abstract
AbstractLow-stress fatigue-crack-propagation tests have been carried out on three commercially pure α-titaniumalloys. It was found that decreasing load ratio (R), increasing grain size, and increasing interstitial alloying content could all produce significant reductions in growth rate over the ∆K range studied (4–20 MN/m2). The conclusion was reached that the fatigue-fracture process comprised two stages: (1) the formation of relatively planar facets (primarily ∆K-controlled) and (2) their interconnection by a mechanism involving plastic tearing (primarily K max-controlled). Scanning electron microscope examination of the fatigue-fracture surfaces revealed that the orientations of individual grains exerted a considerable influence on fracture-surface morphology. This effect occurred when the scale of reversed plasticity at the crack tip was of the order of, or less than, the grain size. A transition in fracturesurface appearance occurred in all specimens at an approximately constant value of growth rate ...
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