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For series (b), more fringes were observed for both specimens.
The T-stress is also negative for both specimens.
Moreover, the displacement time history for both specimens is also obtained by the SODF analysis.
Indeed, the CAA capacity for both specimens had the same resistance elements and mechanisms.
The basis for disregarding the results for these specimens was that the loadings for both specimens were not concentric.
Upon preliminary analysis of the results, it was decided that the results for both specimens C1 (control) and C6 (constant current) to be disregarded.
Similar(38)
NTM were isolated from both specimens for 1 of 61 controls with >1 sample being culture positive for NTM.
Finally, an analytical based, structural stress model was used to generate a master curve to predict the fatigue life of the SPR joints for both specimen types.
The effect of the residual stresses on the fatigue crack behaviour was modelled for both specimen geometries using two approaches: a crack closure approach where the effective stress intensity factor was computed; and a residual stress approach where the effect of the residual stresses on the stress ratio was considered.
Two orientations of specimens were used, chosen so that the influence on the fracture behaviour of the 'ordinary' dislocations (b =a/2 < 110]) and 'superdislocations' (b =a < 101]) could be distinguished.K1c rises steadily from∼1.5MPa m1/2 at 20°C to∼3.5MPa m1/2 at ∼600°C for both specimen types.
A similar time course was observed for both specimen collection days between groups (Table 1).
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