Abstract— A series of crack growth experiments has been preformed on the near alpha titanium alloy, Ti‐1100, to determine the mechanism of the creep‐fatigue interaction. Based on pure creep crack growth results, the increase in the creep‐fatigue crack growth rate is not amenable to separate contributions of creep crack growth and fatigue crack growth. A mechanism has been proposed to account for the increase in creep‐fatigue crack growth rate that is based on the planar slip of titanium alloys which results in the formation of dislocation pileups at the prior beta grain boundaries and leads to intergranular fracture. This mechanism has been validated through crack growth experiments preformed on a Ti‐1100 that has been microstructurally mod...
The mechanisms of low-cycle, fatigue crack nucleation and early growth were investigated at room tem...
High temperature fatigue crack growth experiments were carried out on Ti6242 alloy with large colony...
The high strength-to-weight ratio, good corrosion resistance and retention of good mechanical stabil...
Abstract— A series of crack growth experiments has been preformed on the near alpha titanium alloy, ...
The loading frequency effects on elevated temperature fatigue crack growth behaviour in a new near- ...
This paper examines the influence of microstructure on the crack growth behavior in high temperature...
The fatigue crack growth behavior of Ti-1100 is analyzed at elevated temperatures to evaluate the ef...
A creep-brittle titanium alloy Ti-6242, which is being used for aeroengine applications, was chosen ...
The crack growth behavior of Ti-1100 is investigated for loading frequencies ranging from 30 to 0.00...
An experimental study is conducted to examine the crack tip/microstructure interactions in lamellar ...
The loading frequency effects on elevated temperature fatigue crack growth behavior in a new near-α,...
From service point of view effect of two important parameters, namely, temperature and frequency on...
Dislocation interactions at the crack nucleation site were investigated in near-alpha titanium alloy...
The mechanisms of low-cycle, fatigue crack nucleation and early growth were investigated at room tem...
High temperature fatigue crack growth experiments were carried out on Ti6242 alloy with large colony...
The high strength-to-weight ratio, good corrosion resistance and retention of good mechanical stabil...
Abstract— A series of crack growth experiments has been preformed on the near alpha titanium alloy, ...
The loading frequency effects on elevated temperature fatigue crack growth behaviour in a new near- ...
This paper examines the influence of microstructure on the crack growth behavior in high temperature...
The fatigue crack growth behavior of Ti-1100 is analyzed at elevated temperatures to evaluate the ef...
A creep-brittle titanium alloy Ti-6242, which is being used for aeroengine applications, was chosen ...
The crack growth behavior of Ti-1100 is investigated for loading frequencies ranging from 30 to 0.00...
An experimental study is conducted to examine the crack tip/microstructure interactions in lamellar ...
The loading frequency effects on elevated temperature fatigue crack growth behavior in a new near-α,...
From service point of view effect of two important parameters, namely, temperature and frequency on...
Dislocation interactions at the crack nucleation site were investigated in near-alpha titanium alloy...
The mechanisms of low-cycle, fatigue crack nucleation and early growth were investigated at room tem...
High temperature fatigue crack growth experiments were carried out on Ti6242 alloy with large colony...
The high strength-to-weight ratio, good corrosion resistance and retention of good mechanical stabil...