K I = f(g) σ (πa) .5 f(g) = 1.12- 0.231(a/b) + 10.55(a/b)2 -21.72(a/b)3 + 30.39(a/b)4
KI: Stress Intensity Factor σ: Remote Stress Applied to component a: Crack Length b: Plate Length f(g): Geometry Correction factor