Research Article
Prediction of Fatigue Crack Growth Rate and Stress Intensity Factors Using the Finite Element Method
Table 2
Number of nodes and elements of the specimens in FRANC2D/L and ANSYS APDL 19.2.
| MCTS | FRANC2D/L | ANSYS Mechanical | Nodes | Elements | Nodes | Elements |
| CT01 | 4606 | 2172 | 491691 | 326808 | CT02 | 4594 | 2166 | 1989912 | 1307107 | CT03 | 4598 | 2168 | 1819895 | 1193704 | CT04 | 4634 | 2186 | 1848501 | 1214092 |
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