Identification of the fatigue stress intensity factor threshold for different load ratios R : From fretting fatigue to C(T) fatigue experiments
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OpenAlex topics: Mechanical stress and fatigue analysis · Fatigue and fracture mechanics · Geotechnical Engineering and Underground Structures
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References (31)
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1. Analysis of pad size effects in fretting fatigue using short crack arrest methodologies10.1016/S0142-1123(99)00077-8 ↗
2. Development of a fretting–fatigue mapping concept: the effect of material properties and surface treatments10.1016/j.wear.2009.09.012 ↗
3. The use of notch and short crack approaches to fretting fatigue threshold prediction: theory and experimental validation10.1016/j.triboint.2006.02.033 ↗
4. Introduction of a new sliding regime criterion to quantify partial, mixed and gross slip fretting regimes: correlation with wear and cracking processes10.1016/j.wear.2010.05.002 ↗
5. Stress gradient effect on the crack nucleation process of a Ti–6Al–4V titanium alloy under fretting loading: comparison between non-local fatigue approaches10.1016/j.ijfatigue.2013.03.005 ↗
6. Kitagawa · 1976
7. Introduction of a reverse simulation approach to identify the fatigue stress intensity factor crack arrest threshold from fretting cracking experiments10.1016/j.triboint.2013.10.016 ↗
8. Reverse identification of short–long crack threshold fatigue stress intensity factors from plain fretting crack arrest analysis10.1016/j.engfracmech.2014.11.001 ↗
9. Extension of the unified approach to fatigue crack growth to environmental interactions10.1016/S0142-1123(01)00137-2 ↗
10. Fatigue and crack growth in 7050-T7451 aluminium alloy under constants- and variable-amplitude loading10.1115/1.4007755 ↗
11. A comparative analysis between multiaxial stress and ΔK-based short crack arrest models in fretting fatigue10.1016/j.engfracmech.2012.06.007 ↗
12. ASTM. Standard Test Method for Measurement of Fatigue Crack Growth Rates, vol. E647-13.
13. From uni- to multi-axial fretting–fatigue crack nucleation: development of a stress-gradient-dependent critical distance approach10.1016/j.ijfatigue.2013.05.016 ↗
14. Delacroix J, Cazottes S, Daniélou A, Fouvry S, Buffiere J-Y. Influence of microstructure on the fretting resistance of Al-Cu-Li alloys. Presented at the international conference on aluminium alloys; 2012.10.1002/9781118495292.ch76 ↗
15. ASTM. Standard Test Method for Plane-Strain Fracture Toughness of Metallic Materials, in: E399-90.
16. Fatigue crack growth in the heat affected zone of a hydraulic turbine runner weld10.1016/j.ijfatigue.2014.03.006 ↗
17. Numerical modelling of crack–contact interaction in 2D incomplete fretting contacts using X-FEM10.1016/j.triboint.2009.04.003 ↗
18. A path independent integral and the approximate analysis of strain concentration by notches and cracks10.1115/1.3601206 ↗
19. Influence of R ratio and stick zone eccentricity on the prediction of the fretting fatigue limit with spherical contact10.1016/j.ijfatigue.2006.10.015 ↗
20. On the estimation of fatigue failure under fretting conditions using notch methodologies10.1046/j.1460-2695.2003.00649.x ↗
21. 2D fatigue crack propagation in rails taking into account actual plastic stresses10.1016/j.engfracmech.2014.03.020 ↗
22. Fretting fatigue crack growth simulation based on a combined experimental and XFEM strategy10.1016/j.ijfatigue.2012.07.007 ↗
23. Prediction of fretting crack propagation based on a short crack methodology10.1016/j.engfracmech.2007.06.011 ↗
24. Handbook M. Metallic materials and elastic for aerospace vehicle structures [Online].
25. Analysis of high temperature fatigue crack growth behavior10.1016/S0142-1123(97)00028-5 ↗
26. Fonte M, Stanzl-Tschegg S, Holper B, Tschegg E, Vasudévan A. The environment effect on fatigue crack growth rates in 7049 aluminium alloy at different load ratios, vol. 31; 2003. p. 361–80.10.1016/S1566-1369(03)80020-1 ↗
27. Schijve · 2001
28. The effect of microstructure and environment on fatigue crack growth in 7049 aluminium alloy at negative stress ratios10.1016/S0142-1123(03)00150-6 ↗
29. Some formulas for the crack opening stress level10.1016/0013-7944(81)90034-5 ↗
30. A fatigue crack driving force parameter with load ratio effects10.1016/S0142-1123(01)00158-X ↗
31. Elber W. The significance of fatigue crack closure. Damage tolerance in aircraft structures, ASTM STP 486, American Society for Testing and Materials; 1971. p. 230–42.10.1520/STP26680S ↗