为了研究平均应变对7050-T7451铝合金低周疲劳力学行为的影响,开展了不同应变比(R=-1、-0.06、0.06和0.5)下的室温恒幅低周疲劳试验.结果表明:在对称循环应变下,材料总体表现为循环软化特征;而在非对称循环应变下,材料表现为初始硬化后的循环稳定行为.非对称循环应变导致了材料出现与应变幅相关的平均应力松弛现象.采用Landgraf模型和非线性Maxwell模型分别研究了7050-T7451铝合金的平均应力松弛规律.结果表明:Maxwell模型能够较准确地描述材料的平均应力循环松弛特征,而Landgraf模型更适用于低应变幅下的平均应力松弛描述.
参考文献
[1] | 刘静安;谢水生.铝材在航空航天领域的开发[M].北京:冶金工业出版社,2004:223. |
[2] | 杨守杰,戴圣龙.航空铝合金的发展回顾与展望[J].材料导报,2005(02):76-80. |
[3] | Manson,S.S .Interfaces Between Fatigue,Creep,and Facture[J].International Journal of Fracture Mechanics,1966,2(01):327-363. |
[4] | Attilio Arcari;Norman E. Dowling.Modeling mean stress relaxation in variable amplitude loading for 7075-T6511 and 7249-T76511 high strength aluminum alloys[J].International Journal of Fatigue,2012:238-247. |
[5] | 李雪朝.铝合金材料组织与金相图谱[M].北京:冶金工业出版社,2010:156-159. |
[6] | Fang D;Berkovits A .Mean stress models for low-cycle fatigue of a nickel base supcralloy[J].International Journal of Fatigue,1994,16(06):429-437. |
[7] | Landgraf RW;Chernenkoff RA.Residual stress effects on fatigue of surface processed steels[A].ASTM STP 1004.West Conshohocken,PA:American Society for Testing and Materials,1988:1-12. |
[8] | Jhansale HR;Topper TH.Engineering analysis of the inelastic stress response of a structural metal under variable cyclic strains[A].American Society for Testing and Materials,1973:246-270. |
[9] | Attilio Arcari;Raffaella De Vita;Norman E. Dowling .Mean stress relaxation during cyclic straining of high strength aluminum alloys[J].International Journal of Fatigue,2009(11/12):1742-1750. |
上一张
下一张
上一张
下一张
计量
- 下载量()
- 访问量()
文章评分
- 您的评分:
-
10%
-
20%
-
30%
-
40%
-
50%