AIAA-2006-1673 Fatigue Response of Joint Between Titanium and Titanium Matrix Composite
Fatigue Behavior in Thick Aluminum Panels with a Composite Repair
Effect of Dissimilar Mating Materials on Fretting Fatigue of Ti-6Al-4V
Effect of Shear Force on Fretting Fatigue Behavior of Ti-6Al-4V
Fretting Fatigue Behavior of Ti-6Al-4V Under Displacement Control of Pad
Prediction of Fretting Fatigue Crack Initiation Based on the Plane of Maximum Shear Stress Amplitude
Effect of Disbond on Fatigue Behavior of Cracked Aluminum Panel with Bonded Composite Patch