Research Article
Application of a Cohesive Zone Model for Simulating Fatigue Crack Growth from Moderate to High Levels of Inconel 718
Figure 10
The traction against the number of applied cycles is compared between (a) point 1 and (b) point 4, and the constant loading amplitude is carried out with at , which corresponds to the initial stress intensity factor range for the CT specimen.
(a) |
(b) |