2002, Vol. 16

Issue (5): 547-550 DOI:

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. . Chin J Mater Res, 2002, 16(5): 547-550.

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Received: 01 January 1900

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1 Robert P.Wei,Corrosion and Corrosion Fatigue of Air- frame Materials,DOT/FAA/AR-00/22,2000.
2 JIANG Zuguo,Corrosion Fatigue for Aircraft Structures (Beijing,Aviation Industry Press,1992)p.39 (蒋祖国，飞机结构腐蚀疲劳(北京，航空工业出版社，1992) p．39)
3 J.E.Zamber,B.M.Hillberry,A Probabilistic Approach to Predicting Fatigue Lives of Corroded 2024-T3,AIAA-98- 2054
4 Ruoxue Zhang,Sankaran Mahadevan,Reliability-based reassessment of corrosion fatigue life,Structural Safty,23, 77～91(2001)
5 R.S.Piascik,S.A.Willard,The growth of small corrosion fatigue cracks in alloy 2024,Fatigue and Fracture of En- gineering Materials & Structures,17,1247～1259(1994)
6 A.D.B.Gingell,J.E.King,The effect of frequency and microstructure on corrosion fatigue crack propagation in high strength aluminum alloys,Acta Mater.,45(9), 3855～3870(1997)
7 ZHENG Xiaoling,LI Lingfang,Handbook of Civil Aircraft Structures Durability and Damage Tolerance Design(Bei- jing,Aviation Industry Press,2003)p.288 (郑晓玲主编，民机结构耐久性与损伤容限设计手册(北京，航空工业出版社，2003)p．288)
8 BAO Rui,ZHANG Jianyu,CHEN Bo,FEI Binjun,The up and down method for DFR testing,Journal of Bei- jing University of Aeronautics and Astronautics,30(1), 47(2004) (鲍蕊，张建宇，陈勃，费斌军，试验测定DFR的升降法方法，北京航空航天大学学报，30(1)，47(2004))
9 ZHANG Jianyu,BAO Rui,CHEN Bo,FEI Binjun,Study on DFR method under corrosive environment for fatigue analysis,Journal of Beijing University of Aeronautics and Astronautics,30(6),547(2004) (张建宇，鲍蕊，陈勃，费斌军，腐蚀环境下疲劳分析的DFR疗法研究，北京航空航天大学学报，30(6)，547(2004))
10 GAO Zhentong,Statistics in Fatigue(Beijing,National Defense Industry Press,1986)p.336 (高镇同，疲劳应用统计学[M](北京，国防工业出版社，1986) p．336)
11 D.V.Ramsamooj,T.A.Shugar,Modeling of corrosion fa- tigue in metals in an aggressive environment,International Journal of Fatigue,23,S301-S309(2001)
12 LIU Wenting,YANG Hongyuan,HE Xiaofan,Journal of Beijing University of Aeronautics and Astronautics,8, 753(2004) (刘文廷，杨洪源，贺小帆，北京航空航天大学学报，8，753(2004))
13 M.L.Du,F.P.Chiang,Damage of Al 2024 alloy due to se- quential exposure to fatigue,corrosion and fatigue,Int.J. fatigue,20(10),743(1998)V

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