Stress Intensity Factors for Cracked Finite Plates with Mixed Boundary Condition

Table 2

Calculation parameters for the airfoil-shaped plate.

Crack length	𝑎−𝑏=0.25
Crack tip distance	2𝑏=0.125
Swept back angle	𝛼=20^∘
Number of summation term	𝑀=15
Total number of collocation point	𝑁=384