A Comparison Study of Wear and Fretting Fatigue Behavior Between Cr-alloyed Layer and Cr-Ti Solid-solution Layer
Shou-Ming Yu(
),Dao-Xin Liu(),Xiao-Hua Zhang,Cheng-Song Liu
),Dao-Xin Liu(),Xiao-Hua Zhang,Cheng-Song Liu
.
Fig. 8. Plain fatigue life of Ti6Al4V base material and various surface-treated samples at a stress of 700 MPa
