Abstract

Applying and Validating Fracture Methods to Structural Analysis of Aircraft Components – Practical Issues and Challenges

Applying and Validating Fracture Methods to Structural Analysis of Aircraft Components – Practical Issues and Challenges
By NSE Composites Engineers Bolted/Bonded Joints Fracture & Fatigue January 2, 2004

Applying and Validating Fracture Methods to Structural Analysis of Aircraft Components—Practical Issues and Challenges

Hoyt, D.M., Walker, T.H., Graesser, D.L.

FAA/ASTM Workshop on Computational Fracture Mechanics for Composites, Salt Lake City, UT March 22-23, 2004.