Skip to content
  • About Us
  • Our Work
  • Residual Stress Measurement
    • Contour Method
    • Slitting Method
    • Hole Drilling Method
    • Ring Core Method
    • X-ray Diffraction Method
    • Neutron Diffraction Method
    • 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
  • Our Work
  • Residual Stress Measurement
    • Contour Method
    • Slitting Method
    • Hole Drilling Method
    • Ring Core Method
    • X-ray Diffraction Method
    • Neutron Diffraction Method
    • 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
Previous Image
Next Image

Picture3

Illustration of the F-22 aircraft showing the lugs where the wings attach
Posted on March 17, 2016March 10, 2021Full size 832 × 348

Post navigation

Published inExtending Life of Fighter Airframes
3083 Gold Canal Drive, Suite 100
Rancho Cordova, CA 95670
Tel: (916) 635-5706
Fax: (916) 604-4517