Fatigue crack growth due to spectrum load produced by trains in a bridge
Source abstract
Abstract
• The paper studies FCG due to a load pattern produced by trains crossing a bridge. • Damage accumulation is very irregular along each load block, the major part occurring in the overload region. • The periodic overloads produce significant plasticity induced crack closure. • The overload produces crack tip blunting, enhancing the effect of subsequent load cycles. • The maximum elastic load range was used to eliminate irrelevant load cycles. The present paper studies fatigue crack growth (FCG) produced by a load pattern obtained numerically in a simulation of trains crossing a real bridge. It uses a model where the cyclic plastic deformation is assumed to be the main damage mechanism and that cumulative plastic strain at the crack tip is the driving parameter for FCG. The accumulation of damage was found to be very irregular along each load block, the major part occurring in the overload region. Plasticity induced crack closure is relatively high due to the periodic application of overloads, playing a major role. The overload produces crack tip blunting, increasing the effective load range in subsequent load cycles. The maximum elastic load range was quantified and used to eliminate load cycles not producing fatigue damage, which is important to reduce the numerical effort. The comparison of Finite Element Model (FEM) predictions with NASGRO results, showed that this gives a non-conservative difference of 23% in the number of load cycles after 1 mm of crack growth.
Source: openalex_inverted_index · Quality: baseline
Research context
OpenAlex topics: Fatigue and fracture mechanics · Material Properties and Failure Mechanisms · Railway Engineering and Dynamics
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (41)
Show source-provided references
1. Fatigue crack growth behaviour and life prediction for 2324-T39 and 7050-T7451 aluminium alloys under truncated load spectra10.1016/j.ijfatigue.2009.12.010 ↗
2. Prediction of the fatigue lifetime of the portuguese air force epsilon TB-30 aircraft
3. Experimental validation of railway axle fatigue crack growth using operational loading10.1016/j.engfracmech.2019.04.001 ↗
4. Tavares · 2023
5. Fatigue analysis on the mooring chain of a spread moored FPSO considering the OPB and IPB10.1016/j.ijnaoe.2018.03.004 ↗
6. Lowak H et al. 1979 MINITWIST - A shortened version of TWIST. Report No. TB-146, Laboratorium fur betriebsfestigkeit, Darmstadt.
7. De Jonge JB. 1979 Additional information about FALSTAFF. NLR-TR 79056 U.
8. Edwards PR, Darts J. 1984 Standardized Fatigue loading sequences for helicopter rotors (HELIX and FELIX), Part 2: Final definition of HELIX and FELIX. RAE Technical Report 84085.
9. Cold Turbistan - final definition of a standardized fatigue test loading sequence for tactical aircraft cold section engine disc
10. Fatigue and crack-growth behavior in a titanium alloy under constant-amplitude and spectrum loading10.1016/j.engfracmech.2017.10.036 ↗
11. Fatigue testing and analysis of peened highway bridge welds under in-service variable amplitude loading conditions10.1016/j.ijfatigue.2010.09.004 ↗
12. Fatigue & Fracture Associates. LLC, FASTRAN A Fatigue Crack Growth Life- Prediction Code Based on the Crack-Closure Concept Version 5.4 User Guide. Eupora, MS 39744, 2013.
13. Newman Jr JC. FASTRAN II – A fatigue crack growth structural analysis program. NASA TM 104159; 1992.
14. Harter JA. 2014 AFGROW Users Guide and Technical Manual. Version 2.02.01.18, LexTech.
15. NASGRO reference manual version 5.2. Southwest Research Institute and NASA Johnson Space Center. 2008.
16. Lessons from a fatigue prediction challenge for an aircraft wing shear tie post10.1016/j.ijfatigue.2019.02.007 ↗
17. Numerical simulation of fatigue crack growth based on accumulated plastic strain10.1016/j.tafmec.2020.102676 ↗
18. Numerical prediction of fatigue crack growth based on cumulative plastic strain versus experimental results for AA6082-T610.1007/s10704-022-00680-w ↗
19. Effect of load blocks on fatigue crack growth10.1016/j.ijfatigue.2022.107001 ↗
20. Effect of crack flank holes on fatigue crack growth10.1016/j.ijfatigue.2023.107505 ↗
21. Three-dimensional numerical simulation of the deep-drawing process using solid elements10.1016/S0924-0136(99)00345-3 ↗
22. Plastic instability under plane stress10.1016/0022-5096(52)90002-1 ↗
23. A mathematical representation of the multiaxial Bauschinger effect10.3184/096034007X207589 ↗
24. Fatigue crack propagation analysis in 2024-T351 aluminium alloy using nonlinear parameters10.1016/j.ijfatigue.2021.106478 ↗
25. A numerical study of the effect of single overloads on plasticity induced10.1016/j.tafmec.2016.12.001 ↗
26. ASTM E 647-11. Standard test method for measurement of fatigue crack growth rates. Philadelphia: American Society for Testing and Materials (ASTM); 2011.
27. ISO 12108. Metallic materials – fatigue testing – fatigue crack growth method. Geneva: International Organization for Standardization (ISO); 2012.
28. Estimations of fatigue life and variability under random loading in aluminum Al-2024T351 using strip yield models from NASGRO10.1016/j.ijfatigue.2015.09.031 ↗
29. Numerical prediction of fatigue threshold of metallic materials in vacuum10.1016/j.engfracmech.2019.106491 ↗
30. Elastic correction of fatigue crack growth laws10.1111/ffe.12968 ↗
31. Forman RG, Mettu S R. 1982. Behavior of Surface and Corner Cracks Subjected to Tensile and Bending Loads in Ti-6Al-4V Alloy. Fracture Mechanics: Twenty-second Symposium, Vol. 1, ASTM STP 1131, Ernst HA, Saxena A, McDowell DL eds., American Society for Testing and Materials, Philadelphia:519-546.
32. A crack opening stress equation for fatigue crack growth
33. Cervay RR. 1982 An Empirical Model for Load Ratio and Test Temperature Effects on the Fatigue Crack Growth Rate of Aluminum Alloy 2024-T351, University of Dayton Research Institute, Dayton, OH, Contract No. F33615-80-C-5011, Report No. AFWAL-TR-82-4025. March.
34. Schra L, et al. 1984 Engineering Property Comparisons for 2324-T39 and 2024-T351 Aluminium Alloy Plate, National Aerospace Laboratory, Amsterdam, The Netherlands, NLR TR 84021 U.
35. Fatigue life prediction method for AISI 316 stainless steel under variableamplitude loading considering low amplitude loading below the endurance limit in the ultrahigh cycle regime10.1016/j.ijfatigue.2017.04.006 ↗
36. Mechanisms associated with transient fatigue frack growth under variableamplitude loading: an experimental and numerical study
37. A criterion for omission of variable amplitude loading histories10.1016/0142-1123(86)90025-3 ↗
38. Experimental validation of inspection intervals for railway axles accompanying the engineering process10.1016/j.ijfatigue.2015.09.020 ↗
39. Influence of cyclic loads below endurance limit or threshold stress intensity on fatigue damage in cast aluminium alloy 319-T710.1016/j.ijfatigue.2004.06.004 ↗
40. Effect of underload cycles on oxide-induced crack closure development in Cr-Mo low-alloy steel10.3390/ma14102530 ↗
41. Near-tip strain evolution and crack closure of growing fatigue crack under a single tensile overload10.1016/j.ijfatigue.2020.105478 ↗