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变幅载荷下铝合金的腐蚀疲劳裂纹起始寿命 |
王荣;郑修麟 |
西安石油学院;西安710065;西北工业大学;西安710072 |
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CORROSION FATIGUE CRACK INITIATION LIFE OF AN ALUMINUM ALLOY UNDER VARIABLE AMPLITUDE LOADING |
WANG Rong (Xi'an Petroleum Institute; Xi'an 710065)ZHENG Xiu-lin (Northwestern Polytechnical University; Xi'an 710072) |
1 王荣.铝合金腐蚀疲劳定量规律的研究.西北工业大学博士学位论文,1994.6 2 Hagn L. Mats Sci and Eng, 1988; A103(1):193 3 Akid R. Fract. Mater. Struct. 1996, 19(2/3): 277 4 路民旭,刘晓坤,王建军,郑修鳞.航空学报,1988,9(13):S91 5 王荣,郑修麟,刘文宾.固体力学学报,1995,16(S.Issue):66 6 王荣,郑修麟.中国腐蚀与防护学报,1996,16(4):256 7 Zheng X.-L.Int J.Fatigue,1993,15(6):461 8 郑修麟著.金属疲劳的定量理论.西北工业大学出版社,1994.193 9 Zheng Xiulin. Int. J. Fatigue, 1986, 8(1):17 10 Hirose Y, Mura T. Eng. Fract. Mech., 1985, 22(5): 859 11 蒋祖国主编.飞机结构腐蚀疲劳,北京:航空工业出版社,1992.p.159 |
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