Study of Fatigue Crack Growth Rate of AA6061 at Different Stress Ratios
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Publisher
Springer Singapore
Link
http://link.springer.com/content/pdf/10.1007/978-981-10-6002-1_6
Reference11 articles.
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2. Rodopoulos Chris A, Alexis T (2007) Kermanidis: understanding the effect of block overloading on the fatigue behaviour of 2024-T351 aluminium alloy using the fatigue damage map. Int J Fatigue 29:276–288
3. Jogia BF, Brahmankar PK, Nanda VS, Prasad RC (2008) Some studies on fatigue crack growth rate of aluminum alloy 6061. J Mater Process Technol 201:380–384
4. Thomas WM (1986) The effect of single overloads upon fatigue cracks in 5083-H321 aluminium. Eng Fract Mech 23(6):1015–1029
5. Borrego LP, Ferreira JM, Costa JM (2001) Fatigue crack growth and crack closure in an AlMgSi alloy. Fatigue Fract Eng Mater Struct 24:255–266
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Experimental and simulation analysis of fatigue life of aluminum 6061-T6 alloy;World Journal of Engineering;2022-02-24
2. Estimation of Plastic Zone at Crack Tip Under Fatigue Loading of AA6061-T6 Aluminum Alloy by Finite Element Analysis Using ANSYS;Lecture Notes in Mechanical Engineering;2019
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