Effect of stress ratio and test methods on fatigue crack growth rate for nickel based superalloy Udimet720
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OpenAlex topics: Fatigue and fracture mechanics · High Temperature Alloys and Creep · Probabilistic and Robust Engineering Design
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References (24)
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1. A review of fatigue crack growth characterisation by linear elastic fracture mechanics10.1111/j.1460-2695.1988.tb01219.x ↗
2. The effect of stress ratio and frequency on fatigue crack growth10.1111/j.1460-2695.1979.tb01333.x ↗
3. Crack closure and influence of cycle ratio R on fatigue crack growth in type 304 stainless steel at room temperature10.1016/0013-7944(79)90004-3 ↗
4. Hudson CM. Effect of stress ratio on fatigue crack growth in 7075-T6 and 2024-T3 aluminum alloys specimens, NASA TN-D 5390, 1969.10.1016/0013-7944(69)90003-4 ↗
5. Theodore T, Mall S. Elevated temperature crack growth in aircraft engine materials. In: Advances in fatigue lifetime predictive techniques, ASTM STP 1122, 1992:143–57.10.1520/STP24157S ↗
6. The influence of environment and stress ratio on the low frequency fatigue crack growth behaviour of two medium-strength quenched and tempered steels10.1016/0142-1123(84)90016-1 ↗
7. The influence of mean stress and thickness on fatigue crack growth behaviour in the aluminium alloy BS2L7110.1243/03093247V133129 ↗
8. Effect of ΔK control modes on variability/reproducibility of fatigue crack growth rate data10.1016/0022-3115(92)90419-L ↗
9. A fatigue crack growth theory10.1007/BF00035955 ↗
10. Schijve J. Fatigue crack closure: observations and technical significance. In: Mechanics of fatigue crack closure, ASTM STP 982, 1988:5–34.10.1520/STP27198S ↗
11. The effects of stress ratio, compressive peak stress and maximum stress level on fatigue behaviour of 2024-T3 aluminium alloy10.1111/j.1460-2695.1989.tb00503.x ↗
12. A critical analysis of crack propagation laws10.1115/1.3656900 ↗
13. The effect of load ratio on the m-lnC relationship10.1016/0142-1123(91)90125-I ↗
14. The effect of mean stress on fatigue crack propagation10.1007/BF00033527 ↗
15. Katcher M, Kaplan M. Effect of R-factor and crack closure on fatigue crack growth for aluminium and titanium alloys. In Fracture toughness and slow-stable cracking, ASTM STP 559, 1974:264–82.10.1520/STP38604S ↗
16. Numerical analysis of crack propagation in cyclic loaded structures10.1115/1.3609637 ↗
17. Walker K. The effect of stress ratio during crack propagation and fatigue for 2024-T3 and 7075-T6 aluminium. In: effects of environment and complex load history on fatigue life, ASTM STP 462, 1970:1–14.10.1520/STP32032S ↗
18. Fatigue crack growth under the conjoint action of major and minor stress cycles10.1111/j.1460-2695.1996.tb00961.x ↗
19. Pickard · 1986
20. Brooks RR. Fatigue damage mechanisms in the nickel-based superalloy Udimet 720. PhD thesis, University of Sheffield, February, 1996.
21. Zheng J. Characterisation of the fatigue crack growth behaviour of advanced aero-engine alloys. PhD thesis, University of Portsmouth, January 1998.
22. A method to reduce the scatter in fatigue crack growth rate data10.1111/j.1460-2695.1997.tb01492.x ↗
23. Analysis of fatigue crack propagation data10.1007/BF00049221 ↗
24. Evaluation of fatigue crack growth rate by polynomial curve fitting10.1007/BF00035965 ↗