[1] Sriaman M R, Pidapati R M. Life prediction of aircraft aluminum subjected to pitting corrosion under fatigue condition. Journal of Aircraft, 2009, 46(4): 1253-1259.[2] Merati A. A study of nucleation and fatigue behavior of an aerospace aluminium alloy 2024-T3. International Journal of Fatigue, 2005, 27(10): 33-44.[3] Wang Q Y, Kawagoishi N, Chen Q, et al. Evaluation of the probability distribution of pitting corrosion fatigue life in aircraft materials. Acta Mechanica Sinica, 2003, 19(3): 247-252.[4] Dolley E J, Lee B, We R P. The effect of pitting corrosion on fatigue life. Fatigue & Fracture of Engineering Materials & Structures, 2000, 23(7): 555-560[5] van der Walde K, Hillberry B M. Initiation and shape of development of corrosion-nucleated fatigue cracking. International Journal of Fatigue, 2007, 29(10): 1269-1281.[6] Chubb J P, Morad T A, Hockenhull B S, et al. The effect of exfoliation corrosion on the fracture and fatigue behavior of 7178-T6 aluminium. International Journal of Fatigue, 1995, 17(1): 49-54.[7] Min L, Bombardier Y, Renaud G. Probabilistic risk analysis for aircraft structures with limited in-service damages. 28th International Congress of the Aeronautical Sciences, 2012: 1-11.[8] Liu W T, Li Y H. Aircraft structure calendar life evolution technology. Beijing: Aeronautic Industry Press, 2004. (in Chinese) 刘文珽,李玉海. 飞机结构日历寿命体系评定技术. 北京:航空工业出版社,2004[9] He X F, Liu W T, Jiang D B. Method for fatigue test of aircraft structures considering corrosion influence. Journal of Beijing University of Aeronautics and Astronautics, 2003, 29(1): 20-22. (in Chinese) 贺小帆,刘文珽,蒋东滨. 一种考虑腐蚀影响的飞机结构疲劳试验方法. 北京航空航天大学学报,2003, 29(1):20-22.[10] Zhang F Z, Tan W D, Song J, et al. Effect of corrosion temperature on fatigue life of aircraft. Acta Aeronautica et Astronautica Sinica, 2004, 25(5): 473-475. (in Chinese) 张福泽, 谭卫东, 宋军, 等. 腐蚀温度对飞机疲劳寿命的影响. 航空学报, 2004, 25(5): 473-475.[11] Li Y H, He X F, Chen Q Z, et al. Investigation and variable rule for corrosion depth of aluminum specimen. Journal of Beijing University of Aeronautics and Astronautics, 2002, 28 (1): 98-101. (in Chinese) 李玉海, 贺小帆, 陈群志, 等. 铝合金试件腐蚀深度分布特性及变化规律研究. 北京航空航天大学学报, 2002, 28(1): 98-101.[12] Cui C J, Chen Q Z, Wang Y Y, et al. Corrosion behavior of LY12CZ aluminum alloy in a laboratory simulated atmospheric environment of one airport. Corrosion Science and Projection Technology, 2009, 21(3): 291-294. (in Chinese) 崔常京, 陈群志, 王逾涯, 等. 模拟某机场大气环境下LY12CZ铝合金的腐蚀行为及其当量关系的建立. 腐蚀科学与防护技术, 2009, 21(3): 291-294.[13] Zhang Y H. The corrosion damage and its effect on life of aircraft structure. Xi'an: Northwestern Polytechnical University, 2007. (in Chinese) 张有宏. 飞机结构的腐蚀损伤及其对寿命的影响. 西安:西北工业大学,2007.[14] Chen Y L, Jin P, Lin D X, et al. Naval aircraft structure corrosion control and strength evaluation. Beijing: National Defence Industry Press, 2009. (in Chinese) 陈跃良,金平,林典雄, 等. 海军飞机结构腐蚀控制及强度评估. 北京: 国防工业出版社, 2009.[15] Chen Q Z, Yang R Q, Li G Y, et al. Influence of corrosion on fatigue life of 30CrMnSiNi2A steel structure. Equipment Environment Engineering, 2007, 4(5): 7-10. (in Chinese) 陈群志, 杨瑞琴, 李国元, 等. 腐蚀对30CrMnSiNi2A钢结构疲劳寿命的影响. 装备环境工程, 2007, 4(5): 7-10.[16] Yang X H, Yao W X, Chen Y L. Research calendar life of aircraft structure considering the effects of calendar environment. Chinese Journal of Applied Mechanics, 2002, 19(3): 157-159. (in Chinese) 杨晓华, 姚卫星, 陈跃良. 考虑日历环境影响的结构日历寿命研究. 应用力学学报, 2002, 19(3): 157-159.[17] Fan C H. Study on some critical problem for single aircraft structure life surveillance. Xi'an: Air Force Engineering University, 2010. (in Chinese) 范超华. 飞机结构单机寿命监控若干关键问题研究. 西安: 空军工程大学,2010.[18] Menan F, Henaff G. Influence of frequency and exposure to a saline solution on the corrosion fatigue crack growth behavior of aluminum alloy 2024. International Journal of Fatigue, 2009, 31(33): 1684-1695.[19] Menan F, Henaff G. Synergistic action of fatigue and corrosion during crack growth in the 2024 aluminium alloy. Procedia Engineering, 2010, 2(3): 1441-1450.[20] Xie L Y, Lv W G, Shi Z F. Experimental study on fatigue damage under two level loading. Journal of Mechanical Strength, 1994, 16(3): 589-594. (in Chinese) 谢里阳, 吕文阁, 师照峰. 两级载荷作用下疲劳损伤状态的实验研究. 机械强度, 1994, 16(3): 589-594.[21] Zhang H W, He Y T, Wu L M, et al. Corrosion/fatigue alternative life predicting methodology for aircraft metal structures in consideration of static-stress. Chinese Journal of Applied Mechanics, 2012, 29(5): 589-594. (in Chinese) 张海威, 何宇廷, 伍黎明, 等. 考虑静强度要求的飞机金属结构腐蚀/疲劳交替寿命预测方法. 应用力学学报, 2012, 29(5): 589-594. |