Skip to content
  • About Us
    • Patents
    • Accreditation
  • Our Work
  • Residual Stress Measurement
    • Contour Method
    • Slitting Method
    • Hole Drilling Method
    • Ring Core Method
    • X-ray Diffraction
    • Neutron Diffraction
    • Deep Hole Drilling
    • Barkhausen Noise Analysis
  • Fatigue Analysis & Design
    • Fatigue Engineering
    • Fatigue Life Extension
    • Fatigue Testing and Certification
  • Residual Stress Engineering
    • Distortion Engineering
    • ERS-Toolbox®
    • Fatigue Life Extension
    • Quality Control
  • Blog
  • Contact Us
  • About Us
    • Patents
    • Accreditation
  • Our Work
  • Residual Stress Measurement
    • Contour Method
    • Slitting Method
    • Hole Drilling Method
    • Ring Core Method
    • X-ray Diffraction
    • Neutron Diffraction
    • Deep Hole Drilling
    • Barkhausen Noise Analysis
  • Fatigue Analysis & Design
    • Fatigue Engineering
    • Fatigue Life Extension
    • Fatigue Testing and Certification
  • Residual Stress Engineering
    • Distortion Engineering
    • ERS-Toolbox®
    • Fatigue Life Extension
    • Quality Control
  • Blog
  • Contact Us

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

Post navigation

Published inERS-toolbox® at AFGROW Users Workshop
3083 Gold Canal Drive, Suite 100
Rancho Cordova, CA 95670
Tel: (916) 635-5706
Fax: (916) 604-4517