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Fracture mechanics-based life prediction of a riveted lap joint | ||
Journal of Computational & Applied Research in Mechanical Engineering (JCARME) | ||
مقاله 1، دوره 4، شماره 1، اسفند 2014، صفحه 1-17 اصل مقاله (2.27 M) | ||
نوع مقاله: Research Paper | ||
شناسه دیجیتال (DOI): 10.22061/jcarme.2014.69 | ||
نویسندگان | ||
A. R. Shahani* ؛ H. Moayeri Kashani | ||
Fracture Mechanics Research Laboratory, Department of Applied Mechanics, Faculty of Mechanical Engineering, K.N. Toosi University of Technology, P.O Box 19395-1999, Tehran, Iran | ||
تاریخ دریافت: 25 اردیبهشت 1392، تاریخ بازنگری: 16 اسفند 1392، تاریخ پذیرش: 24 اسفند 1392 | ||
چکیده | ||
In this paper, three-dimensional modeling of the fatigue crack growth profiles was performed in a simple riveted lap joint. Simulation results showed that mode I was dominated on the one side of the plates and the crack straightly grew on this side, while the other side of the plates was in a mixed-mode condition and the crack propagation path was not straight on this side. Afterward, the fracture mechanics-based life prediction of the riveted lap joint was considered using EIFS concept. Back extrapolation method was used for estimating EIFS. Results demonstrated that EIFS would depend on loading amplitude if ΔK had been implemented in EIFS estimation using Paris equation. In contrast EIFS dependency on loading amplitude significantly reduced when using ΔJ in EIFS estimation. Finally, fatigue life of the riveted lap joint was predicted based on safe life method using Brown-Miller critical plane criterion. Results represented that the predicted life using fracture mechanics concept was much closer to the experimental results. | ||
کلیدواژهها | ||
Riveted lap joints؛ Fatigue crack growth profiles؛ EIFS؛ Life prediction | ||
مراجع | ||
[23] P. Moreira, P. Matos and P. Castro, “Fatigue striation spacing and equivalent initial flaw size in Al 2024-T3 riveted specimens”, Theoretical and Applied Fracture Mechanics, Vol. 43, No. 1, pp. 89-99, (2005).
[24] A. Shahani, H. Moayeri Kashani, M. Rastegar and M. Botshekanan Dehkordi, “A unified model for the fatigue crack growth rate in variable stress ratio”, Fatigue and Fracture of Engineering Materials and Structures, Vol. 32, No. 2, pp.105-118, (2009).
[25] J. Draper, Modern Metal Fatigue Analysis, Safe Technology Limited, Sheffield, UK, (2004).
[26] D. Socie and G. Marquis, Multiaxial Fatigue, SAE, USA, (2000).
[27] ASTM-E466, “Standard Practice for Conducting force controlled constant amplitude axial fatigue tests of metallic materials”, Annual Book of ASTM Standards, (1991).
[28] ASTM-E606, “Standard Practice for Strain-Controlled Fatigue Testing”, Annual Book of ASTM Standards, (1998).
[29] C. Boller, and T. Seeger, Material Data for Cyclic Loading-Part D: Aluminum and Titanium Alloys, Material Science Monographs 42D, Elsevier, Amsterdam, (1978). | ||
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