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.

MCTSFRANC2D/LANSYS Mechanical
NodesElementsNodesElements

CT0146062172491691326808
CT024594216619899121307107
CT034598216818198951193704
CT044634218618485011214092