Residual Strength and Fatigue Lifetime of ... - Solid Mechanics
Residual Strength and Fatigue Lifetime of ... - Solid Mechanics
Residual Strength and Fatigue Lifetime of ... - Solid Mechanics
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high growth rate <strong>of</strong> G (see Figure 4.7), but approaching the end <strong>of</strong> 500 cycles with decreasing<br />
G, crack increment becomes smaller. The simulation with qG=q=0.05 follows the reference<br />
simulation with good agreement, but the simulation with qG=q=0.2 shows again less accuracy.<br />
(a)<br />
(b)<br />
Figure 4.8: Crack length vs. number <strong>of</strong> cycles for control parameters (a) qG=q = 0.05 <strong>and</strong> (b)<br />
qG=q = 0.2.<br />
Figure 4.9 presents the phase angle vs. number <strong>of</strong> cycles. The same conclusion may be drawn<br />
upon the accuracy <strong>of</strong> the simulation using the cycle jump method <strong>and</strong> the two control parameters<br />
qG=q=0.05 <strong>and</strong> qG=q=0.2.<br />
(a)<br />
(b)<br />
Figure 4.9: (a) Mode- mixity phase angle vs. number <strong>of</strong> cycles for the reference analysis <strong>and</strong><br />
the analyses with qG=q=0.05 <strong>and</strong> qG=q=0.2 as control parameters.<br />
To measure the computational efficiency <strong>of</strong> the cycle jump method for analyses with different<br />
control parameters, the ratio R is introduced:<br />
N jump<br />
R (4.11)<br />
N<br />
ref<br />
where Njump is the number <strong>of</strong> jumped cycles <strong>and</strong> Nref is the total number <strong>of</strong> cycles in the reference<br />
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