Finite Element Modeling of Crack Generation in Laser Shock Peening Processed Airfoils

<div>(a) The normalized temporal profile, (b) normalized spatial profile of the shock wave for residual stress generation, and (c) normalized spatial profile of the shock wave for crack generation.</div>

Advances in Materials Science and Engineering

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Figure 2

Figure 2: Finite Element Modeling of Crack Generation in Laser Shock Peening Processed Airfoils 