FILIP R,KUBIAK K,ZIAJIA W et al.The effect of microstructure on the mechanical properties of two-phase titanium alloys[J].Journal of Materials Processing Technology,2003,133:84-89.
[3]
LüTJERING G.Influence of processing on microstructure and mechanical properties of α+β titanium alloys[J].Mat Sci Eng A,1998,A243:32-45.
[4]
WANHILL R J H.Ambient temperature crack growth in titanium alloys and its significance for aircraft structures[J].Aeronautical Journal,1977,81:68-82.
[5]
CRICHLOW W J.High cycle fatigue properties of titanium in aircraft application[A].JAFEE R I,BURTE H M (Edited).Titanium Science and Technology[C].New York-London:Plenum Press,1973.1257-1270.
[6]
HINES J A,TJERING G.Propagation of microcracks at stress amplitudes below the conventional fatigue limit in Ti-6A1-4V[J].Fatigue Fract Engng Mater Structure,1999,22:657-665.
