Research Article
Finite Element Modeling of Crack Generation in Laser Shock Peening Processed Airfoils
Figure 7
Simulated residual stress profiles with optimized JC constants ( MPa, MPa, , , and s−1) at (a) 6.7 GPa; (b) 5.3 GPa; (c) 4.2 GPa.
| (a) |
| (b) |
| (c) |