[1] |
谭晓明,陈跃良,段成美. 飞机结构搭接件腐蚀三维裂纹扩展特性分析[J]. 航空学报,2005,26(1):66-69. TAN X M, CHEN Y L, DUAN C M. Analysis of growth characterization of 3-D cracks in corroded lap joints of aircraft structure[J]. Acta Aeronautica et Astronautica Sinica, 2005,26(1):66-69(in Chinese).
|
[2] |
TAN X M, CHEN Y L, JIN P. Corrosion fatigue life prediction of aircraft structure based on fuzzy reliability approach[J]. Chinese Journal of Aeronautics, 2005,18(4):346-351.
|
[3] |
张丹峰,谭晓明,陈跃良. 海洋环境下飞机结构腐蚀疲劳研究现状[J]. 装备环境工程,2009, 6(2):5-8. ZHANG D F, TAN X M, CHEN Y L. Research progress of corrosion fatigue of aircraft structure under marine environment[J]. Equipment Environmental Engineering, 2009, 6(2):5-8(in Chinese).
|
[4] |
BROOKS C L, SIMPSON D. Integrating real time age degradation into the structural integrity process[C]//Proceedings AGARD Workshop on Fatigue in the Presence of Corrosion, 1998.
|
[5] |
贺小帆,梁超.腐蚀退化加速因子模型与分析[J].机械强度,2010,32(2):299-304. HE X F, LIANG C. Model and analysis on the acceleration corrosion factor[J]. Journal of Mechanical Strength, 2010,32(2):299-304(in Chinese).
|
[6] |
李玉海,贺小帆,陈群志. 铝合金试件腐蚀深度分布特性及变化规律研究[J]. 北京航空航天大学学报,2002,28(1):98-101. LI Y H, HE X F, CHEN Q Z. Investigation on distribution and variable rule for corrosion depth of aluminum alloy specimen[J]. Journal of Beijing University of Aeronautics and Astronautics,2002,28(1):98-101(in Chinese).
|
[7] |
李旭东,穆志韬,孔光明.金属腐蚀形貌的分形表征[J].理化检验(物理分册),2014,50(9):639-642. LI X D, MU Z T. KONG G M. Fractal characterization of corrosion morphology of metallic material[J]. Physical Testing and Chemical Analysis(Part A:Physical Testing),2014,50(9):639-642(in Chinese).
|
[8] |
JONES K, SHINDE S R, CLARK P N, et al. Effect of prior corrosion on short crack behavior in 2024-T3 aluminum alloy[J]. Corrosion Science, 2008,50:2588-2595.
|
[9] |
JONES K, HOEPPNER D W. Prior corrosion and fatigue of 2024-T3aluminum alloy[J]. Corrosion Science, 2006,48:3109-3122.
|
[10] |
BIRBILIS N, CAVANAUGH M K, BUCHHEIT R G. Electrochemical behavior and localized corrosion associated with Al7Cu2Fe particlesin aluminum alloy 7075-T651[J]. Corrosion Science, 2006,48:4202-4215.
|
[11] |
HARLOW D G, ROBERT P W. Probability modeling and material microstructure applied to corrosion and fatigue of aluminum and steel alloys[J]. Engineering Fracture Mechanics,2009,76:695-708.
|
[12] |
陈跃良,卞贵学,衣林,等. 腐蚀和疲劳交替作用下飞机铝合金疲劳性能及断裂机理研究[J].机械工程学报,2010,48(20):70-76. CHEN Y L, BIAN G X, YI L, et al. Research on fatigue characteristic and fracture mechanics of aluminum alloy under alternate action of corrosion and fatigue[J]. Journal of Mechanical Engineering, 2010,48(20):70-76(in Chinese).
|
[13] |
谭晓明,张丹峰,卞贵学,等. 腐蚀对新型高强度铝合金疲劳裂纹萌生机制及扩展行为的作用研究[J].机械工程学报,2014,50(20):76-83. TAN X M, ZHANG D F, BIAN G X. Effect of corrosion damage on fatigue crack initiation mechanism and growth behavior of high strength aluminum alloy[J]. Journal of Mechanical Engineering, 2014,50(20):76-83(in Chinese).
|
[14] |
谭晓明,张丹峰,陈跃良. 基于微观结构的2B06铝合金全寿命概率模拟[J].航空学报,2012,33(8):1434-1439. TAN X M, ZHANG D F, CHEN Y L. Probabilistic simulation approach for holistic life of aluminum alloy 2B06 based on material microstructure[J]. Acta Aeronautica et Astronautica Sinica, 2012,33(8):1434-1439(in Chinese).
|
[15] |
QUESNAY D L, UNDERHILL P R, BRITT H J. Fatigue crack growth from corrosion damage in 7075-T6511aluminium alloy under aircraft loading[J]. International Journal of Fatigue, 2003,25:371-377.
|
[16] |
JONES K, HOEPPNER D W. The interaction between pitting corrosion, grain boundaries, and constituent particles during corrosion fatigue of 7075-T6 aluminum alloy[J]. International Journal of Fatigue, 2009,31:686-692.
|
[17] |
NEWMAN J C J. Fatigue-life calculations on pristine and corroded open-hole specimens using small-crack theory[J]. International Journal of Fatigue, 2009,31:1246-1253.
|
[18] |
刘建华,田帅,李松梅,等. 新型超高强度钢应力腐蚀断裂行为研究[J].航空学报, 2011,32(6):1164-1170. LIU J H, TIAN S, LI S M, et al. Stress corrosion crack of new ultrahigh strength steel[J].Acta Aeronautica et Astronautica Sinica, 2011,32(6):1164-1170(in Chinese).
|
[19] |
张晓云,刘明,汤智慧,等. 40CrNi2Si2MoVA超高强度钢海洋大气环境腐蚀行为研究[J]. 腐蚀科学与防护技术,2014,26(5):413-419. ZHANG X Y, LIU M, TANG Z H, et al. Marine atmospheric corrosion of 40CrNi2Si2MoVA high strength steel[J]. Corrosion Science and Protection Technology,2014,26(5):413-419(in Chinese).
|
[20] |
李松梅,吴凌飞,刘建华. 应力比和腐蚀环境对超高强度钢AerMet100疲劳裂纹扩展的影响[J].航空材料学报,2014,34(3):74-80. LI S M, WU L F, LIU J H. Effect of load ratio and corrosion on fatigue behavior of AerMet100 ultrahigh strength steel[J]. Journal of Aeronautical Materials, 2014,34(3):74-80(in Chinese).
|
[21] |
刘文珽,李玉海. 飞机结构日历寿命体系评定技术[M].北京:航空工业出版社,2004. LIU W T, LI Y H. The calendar life system evaluation technology of aircraft structures[M]. Beijing:Aviation Industry Press,2004(in Chinese).
|
[22] |
中国国家标准化管理委员会.金属材料-疲劳试验-轴向力控制方法:GB/T 3075-2008[S]. 北京:中国国家标准化管理委员会2008. Standardization Administration of China. Metallic materials-fatigue testing-axial force controlled method:GB/T 3075-2008[S]. Beijing:Standardization Administration of China,2008(in Chinese).
|
[23] |
中国国家标准化管理委员会. 金属平均晶粒度测定方法:GB/T 6394-2017[S]. 北京:中国国家标准化管理委员会,2017. Standardization Administration of China. Determination of estimating the average grain size of metal:GB/T 6394-2017[S]. Beijing:Standardization Administration of China,2017(in Chinese).
|