Table 4 Crack initiation Angle of upper wing and lower wing.
Pre-existing crack inclination angle (β)/° | 0 | 30 | 60 | 90 |
|---|---|---|---|---|
Crack initiation angle of upper wing(α1)/° | 82.875 | 59.140 | 45.862 | 12.053 |
Crack initiation angle of lower wing(α2)/° | 81.959 | 66.500 | 38.083 | 7.300 |