Crack initiation and lifetime assessment of MAR-M247 nickel-based superalloy in the very high cycle fatigue regime at 550 ℃
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OpenAlex topics: Fatigue and fracture mechanics · High Temperature Alloys and Creep · Aluminum Alloy Microstructure Properties
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References (52)
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1. Morad A, Shash Y. Nickel base superalloys used for aero engine turbine blades. The International Conference on Applied Mechanics and Mechanical Engineering, Military Technical College 2014:1-22.10.21608/amme.2014.35549 ↗
2. On the modelling of precipitation kinetics in a turbine disc nickel based superalloy10.1016/j.actamat.2020.03.058 ↗
3. Strain-rate insensitive yield strength and deformation mechanisms of Ni-base superalloy CM247LC at 600°C10.1016/j.jallcom.2020.158478 ↗
4. High temperature creep behaviour of cast nickel-based superalloys INC 713 LC, B1914 and MAR-M24710.3390/met11010152 ↗
5. Di Gianfrancesco · 2016
6. Elucidating the effects of solution and double ageing treatment on the mechanical properties and toughness of MAR-M247 superalloy at high temperature10.1016/j.matchemphys.2007.11.041 ↗
7. Numerical simulation and high cycle fatigue behaviour study on shot peening of MAR-M247 nickel-based alloy10.1016/j.ijfatigue.2024.108161 ↗
8. Jiang Y, Zou T, Liu M, Wang Q, Pei Y, Zhang H, Liu Y, Wang Q. Tensile deformation behaviors and microstructure evolution under various temperatures for MAR‐M247 nickel‐based superalloy. Adv Eng Mater (2024).10.1002/adem.202302056 ↗
9. Low cycle fatigue behavior of MAR-M247 nickel-based superalloy from 500 to 900°C: analysis of cyclic response, microstructure evolution and failure mechanism10.1016/j.ijfatigue.2024.108564 ↗
10. The effect of laser shock peening with different power density on the microstructure evolution and mechanical properties of MAR-M247 nickel-base alloy10.1016/j.jmrt.2024.04.107 ↗
11. Thermomechanical and isothermal fatigue properties of MAR-M247 superalloy10.1016/j.tafmec.2024.104443 ↗
12. The low cycle fatigue behaviour of MAR-M247 superalloy under different strain rates and cycle shapes at 750°C10.1016/j.ijfatigue.2022.107133 ↗
13. High cycle fatigue in aircraft gas turbines—an industry perspective10.1007/BF00012667 ↗
14. Very high cycle fatigue of a notched Ni-based single crystal superalloy at high temperature10.1016/j.ijfatigue.2024.108379 ↗
15. High cycle fatigue in a single crystal superalloy: time dependence at elevated temperature10.7449/2004/Superalloys_2004_657_666 ↗
16. Propensities of crack interior initiation and early growth for very-high-cycle fatigue of high strength steels10.1016/j.ijfatigue.2013.02.023 ↗
17. Ultrasonic fatigue of a single crystal Ni-base superalloy at 1000°C10.1016/j.msea.2006.08.028 ↗
18. Very high cycle fatigue of Ni-based single-crystal superalloys at high temperature10.1007/s11661-018-4672-6 ↗
19. Transition from internal to surface crack initiation of a single-crystal superalloy in the very-high-cycle fatigue regime at 1100°C10.1016/j.ijfatigue.2021.106343 ↗
20. Fatigue strength of a single crystal in the gigacycle regime10.1016/j.ijfatigue.2007.04.003 ↗
21. Transition behavior from Mode I cracking to crystallographic cracking in a Ni-base single crystal superalloy10.1016/j.ijfatigue.2019.105400 ↗
22. Crack initiation mechanisms during very high cycle fatigue of Ni-based single crystal superalloys at high temperature10.1016/j.actamat.2020.02.012 ↗
23. Orientation dependence of nickel-based single crystal superalloys in VHCF regime10.1016/j.ijfatigue.2024.108502 ↗
24. Crack initiation anisotropy of Ni-based SX superalloys in the very high cycle fatigue regime
25. Crystallographic fatigue crack initiation in nickel-based superalloy René 88DT at elevated temperature10.1016/j.actamat.2009.08.022 ↗
26. Analysis of microdamage in a nickel‐base alloy during very high cycle fatigue10.1111/ffe.12412 ↗
27. Competing modes for crack initiation from non-metallic inclusions and intrinsic microstructural features during fatigue in a polycrystalline nickel-based superalloy10.1007/s11661-018-4780-3 ↗
28. Characterization on crack initiation and early propagation region of nickel-based alloys in very high cycle fatigue10.3390/ma15175806 ↗
29. Lashari MI, Li W, Hu ZF, Li C, Cao XB, Jin YZ. Temperature effect-related high and very high cycle fatigue failure analysis and life estimation of forged superalloy. Met Mater Int; 2025.10.1007/s12540-025-01912-z ↗
30. Failure mechanism and life correlation of Inconel 718 in high and very high cycle fatigue regimes10.1016/j.ijfatigue.2023.107764 ↗
31. Microstructural evolution and formation of fine grains during fatigue crack initiation process of laser powder bed fusion Ni-based superalloy
32. Effect of inclusion on subsurface crack initiation and gigacycle fatigue strength10.1016/S0142-1123(02)00037-3 ↗
33. A two-parameter model to predict fatigue life of high-strength steels in a very high cycle fatigue regime10.1007/s10409-015-0451-4 ↗
34. Fatigue life and mechanistic modeling of interior micro-defect induced cracking in high cycle and very high cycle regimes10.1016/j.actamat.2018.07.036 ↗
35. Incoordination between urban expansion and urban population growth and their interaction
36. Comparison of the very high cycle fatigue behaviors of INCONEL 718 with different loading frequencies10.1007/s11433-013-5013-9 ↗
37. A unified rule for high-cycle and low-cycle fatigue life prediction in multi-scale framework10.1016/j.ijfatigue.2023.107512 ↗
38. Ultrasonic fatigue performance of high temperature structural material Inconel 718 alloys at high temperature after UNSM treatment10.1111/ffe.12330 ↗
39. Fatigue and fracture behavior of nickel-based superalloy Inconel 718 up to the very high cycle regime10.1631/jzus.A1000171 ↗
40. .
41. Telesman J, Ghosn LJ. Fatigue crack growth behavior of PWA 1484 single crystal superalloy at elevated temperatures. In: ASME 1995 International Gas Turbine and Aeroengine Congress and Exposition; 1995.10.1115/95-GT-452 ↗
42. Resolved shear stress intensity coefficient and fatigue crack growth in large crystals10.1016/0167-8442(88)90003-1 ↗
43. Very high cycle fatigue behavior of a directionally solidified Ni-base superalloy DZ410.3390/ma11010098 ↗
44. Microtwinning in Ni-base supalloy Mar-M247 at intermediate temperature and low stress10.1016/j.matlet.2021.129426 ↗
45. The effects of microstructure and microtexture generated during solidification on deformation micromechanism in IN713C nickel-based superalloy10.1016/j.actamat.2018.01.062 ↗
46. Gigacycle fatigue of metallic aircraft components10.1016/j.ijfatigue.2009.03.015 ↗
47. Fatigue variability of a single crystal superalloy at elevated temperature10.1016/j.ijfatigue.2009.03.013 ↗
48. Benefits of high gradient solidification for creep and low cycle fatigue of AM1 single crystal superalloy10.1016/j.msea.2015.07.045 ↗
49. Multiaxial fatigue: an overview and some approximation models for life estimation10.1016/j.ijfatigue.2011.01.003 ↗
50. VHCF life evolution after microstructure degradation of a Ni-based single crystal superalloy10.1016/j.ijfatigue.2017.07.021 ↗
51. Effects of defects, inclusions and inhomogeneities on fatigue strength10.1016/0142-1123(94)90001-9 ↗
52. Defect tolerant design of automotive components10.1016/S0142-1123(96)00079-5 ↗