Estimation of Plastic Zone at Crack Tip Under Fatigue Loading of AA6061-T6 Aluminum Alloy by Finite Element Analysis Using ANSYS
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Publisher
Springer Singapore
Link
http://link.springer.com/content/pdf/10.1007/978-981-13-6469-3_55
Reference9 articles.
1. Verma RP, Pandey KN (2018) Study of fatigue crack growth rate of AA6061 at different stress ratios. In: Seetharamu S, Bhanu K, Raghunath SR, Khare W (eds) FatigueDurability 2017. LNME, Springer, Singapore, pp 67–74. https://doi.org/10.1007/978-981-10-6002-1_6
2. Stanzl-Tschegg SE, Mayer H (2001) Fatigue and fatigue crack growth of aluminium alloys at very high numbers of cycles. Int J Fatigue 23:231–237
3. Benrahou KH, Benguediab M, Belhouari M, Nait-Abdelaziz M, Imad A (2007) Estimation of the plastic zone by finite element method under mixed mode (I and II) loading. Comput Mater Sci 38(4):595–601
4. Paul SK (2016) Numerical models of plastic zones and associated deformations for a stationary crack in a C(T) specimen loaded at different R-ratios. Theoret Appl Fract Mech 84:183–191
5. Park HB, Kim KM, Lee BW (1996) Plastic zone size in fatigue cracking. Int J Press Vessel Pip 68(3):279–285
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