## Abstract High temperature fatigue in nickelβbase superalloys for aeroβengine applications requires consideration of cycleβ and timeβdependent phenomena. For waveforms with dwells and/or low frequencies crack growth rates may be significantly accelerated up to the point of fully timeβdependent cr
The effects of environment and loading waveform on fatigue crack growth in Inconel 718
β Scribed by M.R Bache; W.J Evans; M.C Hardy
- Publisher
- Elsevier Science
- Year
- 1999
- Tongue
- English
- Weight
- 950 KB
- Volume
- 21
- Category
- Article
- ISSN
- 0142-1123
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β¦ Synopsis
The influence of environment and fatigue waveform shape on crack growth behaviour has been evaluated in a workhorse turbine disc material, Inconel 718, at 600Β°C through an experimental programme that investigated crack growth from a notch geometry. Crack growth data are presented for a variety of stress and air pressure conditions, with specific combinations typifying model component test conditions of particular interest. The effect of waveform characteristics covering a range of loading/unloading rates and different dwell periods at peak stress was evaluated. The rates of propagation and the resultant crack profiles were found to be significantly affected by the environmental conditions through control of the dominant fracture mechanisms of transgranular and intergranular cracking. Evidence for environment controlled fatigue crack growth is presented.
π SIMILAR VOLUMES
A theory of fatigue crack growth based on the concept of damage accumulation is presented which takes some account of the effect of periodic-random loading. The Dugdale model of plasticity is used to calculate the distribution of the energy dissipated during stress cycling in the plastic zones of a
A modification to the model of Weir ef al. for surface reaction and transport controlled fatigue crack growth has been developed to explicitly account for the effect of load ratio on environmentally assisted fatigue crack growth. Load ratio was found to affect principalfy gas transport to the crack
## Abstract In titanium alloys an effect of hold time at maximum load in a cyclic test is observed if K~max~ exceeds the threshold for crack propagation at a constant load test. For tests in air it is possible to predict crack growth rate for a hold time cycle from the crack growth rates from a cyc