1995
DOI: 10.1080/01418619508239929
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An electron microscope study of deformation and crack propagation in (α2+ γ) titanium aluminides

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Cited by 61 publications
(14 citation statements)
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“…The process was found to be closely related to mismatch structures and coherency stresses present at the semicoherent interfaces. [3,8,18,23,24] The coherency stresses are comparable with the yield stress of the material and give rise to the formation of loop structures adjacent to the interfaces (Fig. 1c).…”
Section: Generation Of Perfect Dislocationsmentioning
confidence: 67%
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“…The process was found to be closely related to mismatch structures and coherency stresses present at the semicoherent interfaces. [3,8,18,23,24] The coherency stresses are comparable with the yield stress of the material and give rise to the formation of loop structures adjacent to the interfaces (Fig. 1c).…”
Section: Generation Of Perfect Dislocationsmentioning
confidence: 67%
“…[17] At room temperature multiplication has been found to be closely related to jogs in screw dislocations, which were probably generated by cross slip. [3,18] Possible mechanisms are schematically sketched in Figure 3a. Since the jogs are immobile in the direction of the motion of the screw dislocations, dislocation dipoles are trailed at the jogs.…”
Section: Generation Of Perfect Dislocationsmentioning
confidence: 99%
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“…It is possible for in situ SEM measurements of stable crack growth to be made with micromechanical methods [105]. However, for meaningful FCG data to be achieved, the plastic zone should be considerably smaller than the testpiece dimensions, and though this is achievable for brittle ceramics [105], the plastic zone radius of γ -TiAl alloys in fatigue is several microns [106], which is at the limit for a micromechanical testpiece.…”
Section: Fatigue Of Polysynthetically Twinned Crystalsmentioning
confidence: 99%
“…The study of the HCF behaviour of γ -TiAl alloys has generally focused on plasticity in the region of a crack tip, rather than in the bulk of the material [66,106]. This is possibly because in common engineering alloys, achieving HCF loading to over 10 7 cycles often means operating at stresses considerably below the yield stress, so that to exceed the local critical resolved shear stress for slip, stress concentration at a crack tip, a hard particle or a crystal boundary is required.…”
Section: Towards a Microscopic Model For Hcf Loading Of Tial Alloys: mentioning
confidence: 99%