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Comparison of experimental and computed tensile creep curves for a single crystal of orientation 0 0 1. The experimental creep curve is obtained for constant nominal stress creep loading and the computed creep curves are shown for both constant nominal stress (CNS) and constant true stress (CTS) creep loading. The computed curves are for a fully dense material.

Comparison of experimental and computed tensile creep curves for a single crystal of orientation 0 0 1. The experimental creep curve is obtained for constant nominal stress creep loading and the computed creep curves are shown for both constant nominal stress (CNS) and constant true stress (CTS) creep loading. The computed curves are for a fully dense material.

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Experimental observations on tensile specimens in Srivastava et al (2012 in preparation) indicated that the growth of initially present processing induced voids in a nickel-based single crystal superalloy played a significant role in limiting creep life. Also, creep tests on single crystal superalloy specimens typically show greater creep strain ra...

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Context 1
... N = 5 and the parameters used in equation (22) are β ss = 0.998 and t 0 = 1.35 × 10 4 s. Figure 2 shows the experimental tensile creep curve of l/ l 0 versus time, where l 0 is the initial length of the specimen gauge section and l is the change in length of the gauge section with the loading applied in the 0 0 1 direction. For comparison purposes two computed curves for a fully dense material using the parameter values given above are also plotted: one with constant nominal stress and one with constant true stress. ...
Context 2
... corresponds to E e = 0.061 for χ = 3 and L = −1 and to E e = 0.058 for χ = 0.33 and L = −1. The steady-state effective creep strain rate, ˙ E ss , is essentially independent of the value of the Lode parameter and is almost same for χ 0.75 as for the fully dense material in figure 2 which is ˙ E ss = 0.235 × 10 −7 s −1 . For greater values of the stress triaxiality χ there is an effect of χ on ˙ E ss with ˙ E ss increasing to ˙ E ss = 0.438 × 10 −7 s −1 for χ = 3. ...
Context 3
... particular, the responses for L = −1 and L = 1 differ significantly. The steady-state effective strain rate for a fully dense material with constant N 1 in figure 2 is ˙ E ss = 0.355×10 −7 s −1 . There is a small effect of porosity (with f 0 = 0.01) on the steady-state creep rate for χ = 0.33; ˙ E ss = 0.395 × 10 −7 s −1 for χ = 0.33 and L = −1. ...

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... For example, for a porous material, with matrix exhibiting tension-compression asymmetry, the F.E. results obtained using cubic unit-cells showed the importance of the matrix tension-compression asymmetry on the rate of void growth and confirm the predictions of the dilatational model of Cazacu-Stewart [7]. Moreover, anisotropy and creep in porous crystals were investigated with cubic unit-cells in [4] and the results were further explained using an analytical model for porous crystals in [5]. The F.E. results provide insights on the effects of stress triaxiality and Lode parameter on void evolution for ductile single crystals in the dislocation creep. ...
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... with the c M [i] given by (53), and the stress variablesτ ...
... In addition, we can see that f /f 0 grows faster for larger values of X σ in the range X σ > 0, while f /f 0 decreases faster for smaller values of X σ in the range X σ < 0, as expected. Furthermore, the ISO results for f /f 0 are in good qualitative agreement with the corresponding FEM results for X σ > 0. In this context, it should be noted that, in addition to the FEM results of Srivastava and Needleman (2015) (depicted with solid circles), the corresponding FEM results of Srivastava and Needleman (2012) are also shown in Fig. 5(a) (with cross symbols) for X σ = 3 and 1/3 (X σ = 2/3 was not considered by Srivastava and Needleman (2012)). It can be seen that, while for X σ = 1/3 the two sets of FEM results are rather similar, for X σ = 3 they are somewhat different. ...
... In particular, for X σ = 3, the porosities for both the ISO and FEM increase rapidly with strain (see Fig. 5(a)) and, hence, the effect of the void distribution becomes progressively more significant. As pointed out by Srivastava and Needleman (2012), the increase of w at larger strains in the FEM simulation is induced by the necking of the inter-void ligament in the x 1 and x 2 directions (simultaneously), leading to rapid increases of the void radii in these directions. However, there is no well-defined inter-void ligaments for random microstructures and such "local" effects can not be captured by the ISO homogenization model. ...
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... To detect the onset of void coalescence we use the procedure outlined in Srivastava and Needleman (2012), which is based on monitoring the evolution of the relative inter-void ligament size. Since for an isotropic material, the greatest reduction in ligament size occurs in the direction of minimum applied stress, the evolution of the relative inter-void ligament size in the x direction i.e. l r 1 ¼ l 1 =l 0 1 ¼ ðC 1 À r 1 Þ=ðC 0 1 À r 0 Þ with the macroscopic effective strain E e was examined ( Fig. 6(a)). ...