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HE-B-0052-1

Image of the predicted residual stress and distortion in a turbine engine airfoil from laser shock peening

Illustration of predicted residual stress and deformation from application of laser shock processing to a compressor airfoil

Posted on September 6, 2017August 9, 2021Full size 550 × 737

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Published inERS-toolbox® at AFGROW Users Workshop
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