A turbine engine blade alloy (Ti‐8Al‐1Mo‐1V) under different heat treatment conditions was
employed to conduct ultrasonic fatigue tests to investigate the influence of the colony content …

Ultrasonic fatigue tests were carried out to investigate the effect of stress ratio on the very
high cycle fatigue (VHCF) behaviors of titanium alloy (Ti-8Al-1Mo-1V). The fatigue strength …

Ultrasonic fatigue tests were conducted at the stress ratios of− 1,− 0.5,− 0.1, 0.1 and 0.5 for a
Ti–6Al–4V alloy in high-cycle and very-high-cycle fatigue regimes. Experimental results …

In order to investigate the stress ratio effect on notched fatigue behavior of a turbine engine
blade titanium alloy (Ti-8Al-1Mo-1V), notched specimens were employed to perform …

In order to better understand the large scatter in the fatigue results associated with β-
annealed microstructures of α+ β titanium alloys, the fatigue crack initiation and propagation …

Titanium alloys have been widely used as superior engineering materials because of their
high specific strength, high temperature resistance and high corrosion resistance. In their …

The fatigue behaviour of a titanium alloy Ti‐6Al‐4V with equiaxed microstructure (EM) under
different values of tensile mean stress or stress ratio (R) was investigated from high‐cycle …

The effects of stress ratio on high-cycle fatigue (HCF) and very-high-cycle fatigue (VHCF)
behavior of a Ti–6Al–4V alloy were systematically investigated in this paper. Fatigue tests …

The high-cycle fatigue (HCF) of titanium alloy turbine engine components remains a
principal cause of failures in military aircraft engines. A recent initiative sponsored by the …

The behavior of crack initiation and early growth in high-cycle fatigue (HCF) and very-high-
cycle fatigue (VHCF) regimes for a TC4 titanium alloy with equiaxed microstructure was …