A modified model to depict corrosion fatigue crack growth behavior for evaluating residual lives of aluminum alloys
Source abstract
Abstract
A modified Trantina–Johnson model was developed to characterize corrosion fatigue crack growth behavior. Crack growth accumulative methodology based on the Willenborg–Chang rule was used to evaluate the residual lifetimes of corrosion fatigue crack growth. Fatigue crack growth tests were performed on 2524-T3 and 7050-T7451 aluminum alloys subjected to constant amplitude and random spectra loading under the environments of dry air and 3.5% NaCl sodium chloride solution, and the load–environment interaction and load interaction mechanisms were deduced from fractographic analysis. The developed models showed good correlation with experimental results.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Fatigue and fracture mechanics · Hydrogen embrittlement and corrosion behaviors in metals · Material Properties and Failure Mechanisms
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (38)
Show source-provided references
1. Pit-to-crack transition in pre-corroded 7075-T6 aluminum alloy under cyclic loading10.1016/j.corsci.2004.10.004 ↗
2. The interaction between pitting corrosion, grain boundaries, and constituent particles during corrosion fatigue of 7075-T6 aluminum alloy10.1016/j.ijfatigue.2008.03.016 ↗
3. Life prediction of aircraft aluminum subjected to pitting corrosion under fatigue conditions10.2514/1.40481 ↗
4. Initiation and shape development of corrosion-nucleated fatigue cracking10.1016/j.ijfatigue.2006.10.010 ↗
5. Effect of corrosion severity on fatigue evolution in Al–Zn–Mg–Cu10.1016/j.corsci.2009.10.006 ↗
6. Effect of prior corrosion state on the fatigue small cracking behavior of 6151-T6 aluminum alloy10.1016/j.corsci.2011.09.025 ↗
7. Corrosion fatigue behavior and fracture mechanisms in nitride low alloy steel10.1046/j.1460-2695.2003.00572.x ↗
8. Fatigue and damage tolerance behavior of corroded 2024 T351 aircraft aluminum alloy10.1016/j.tafmec.2004.12.008 ↗
9. Corrosion fatigue of a 12% Cr low pressure turbine blade steel in simulated service environments10.1016/j.ijfatigue.2005.06.031 ↗
10. Effect of corrosion on the high cycle fatigue strength of martensitic stainless steel X12CrNiMoV12-310.1016/j.ijfatigue.2012.09.018 ↗
11. Corrosion fatigue behaviors of steel wires used in coalmine10.1016/j.matdes.2013.06.059 ↗
12. Transition from pitting to fatigue crack growth: modeling of corrosion fatigue crack nucleation in a 2024-T3 aluminum alloy10.1016/S0921-5093(96)10414-7 ↗
13. Study on the mechanism of high-cycle corrosion fatigue crack initiation in X80 steel10.1016/j.corsci.2011.12.029 ↗
14. Fatigue and damage tolerance behaviour of corroded 2024 T351 aircraft aluminum alloy10.1016/j.tafmec.2004.12.008 ↗
15. Effect of prior corrosion on short crack behavior in 2024-T3 aluminum alloy10.1016/j.corsci.2008.06.039 ↗
16. A fracture model of corrosion fatigue crack propagation of aluminum alloys based on the material elements fracture ahead of a crack tip10.1016/j.ijfatigue.2007.10.007 ↗
17. Fatigue crack initiation and growth on a steel in the very high cycle regime with sea water corrosion10.1016/j.engfracmech.2010.02.015 ↗
18. Corrosion fatigue crack propagation of an aluminum alloy under periodic overloads10.1111/j.1460-2695.2011.01630.x ↗
19. Investigation on corrosion fatigue crack growth rate in 7075 aluminum alloy10.1016/j.matdes.2013.04.097 ↗
20. Corrosion fatigue crack growth of AISI 4340 steel10.1016/j.ijfatigue.2012.10.015 ↗
21. Corrosion fatigue crack growth behavior of oil-grade nickel-base alloy 718. Part 1: Effect of corrosive environment10.1016/j.corsci.2014.08.022 ↗
22. Fatigue crack growth from corrosion damage in 7075-T6511 aluminium alloy under aircraft loading10.1016/S0142-1123(02)00168-8 ↗
23. Corrosion fatigue in 7075-T6 aluminum: life prediction issues for carrier-based operations10.2514/1.9334 ↗
24. Prediction of corrosion fatigue lives of aluminium alloy on the basis of corrosion pit growth law10.1111/j.1460-2695.2006.01018.x ↗
25. Fatigue life calculations on pristine and corroed open-hole specimens using small-crack theory10.1016/j.ijfatigue.2009.01.007 ↗
26. EIFS-based crack growth fatigue life prediction of pitting-corroded test specimens10.1016/j.engfracmech.2010.03.018 ↗
27. Reliability-based minimal sample factor formulation for corrosion damage assessment in aluminium alloy plates10.1243/030932405X31019 ↗
28. On the initiation and growth behavior of corrosion pits during corrosion fatigue process of industrial pure aluminum10.1016/j.ijfatigue.2007.11.004 ↗
29. Effect of cyclic crack opening displacement rate on corrosion fatigue crack velocity and fracture mode transitions for Al–Zn–Mg–Cu alloys10.1016/j.corsci.2013.12.014 ↗
30. Fatigue cracking from a corrosion pit in an aircraft bulkhead10.1016/j.engfailanal.2014.01.020 ↗
31. A critical analysis of crack propagation laws10.1115/1.3656900 ↗
32. Probabilistic defect size analysis using fatigue and cyclic crack growth rate data
33. The effect of stress ratio during crack propagation and fatigue for 2024-T3 and 7075-T6 aluminum
34. Numerical analysis of crack propagation in cyclic loaded structures10.1115/1.3609637 ↗
35. A crack opening equation for fatigue crack growth10.1007/BF00020751 ↗
36. Xiong · 2011
37. Random spectrum fatigue crack life predictions with or without considering load interactions
38. ASTM · 2011