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以腐蚀深度衡量铝合金的腐蚀损伤,假设蚀坑深度服从对数正态分布、腐蚀深度与腐蚀时间的关系为幂函数式,建立了加速腐蚀因子模型,给出了常用铝合金加速腐蚀因子的表达式;得到了加速腐蚀因子与腐蚀时间无关的结论.并建立了加速腐蚀因子估计值的分布特性和统计分析方法.

参考文献

[1] ROBERT P;WEI D;GARY Harlow .Corrosion and fatigue of aluminum alloys:chemistry micromechanics and reliability[AFRL-SR-BL-TR-01-0569][R].,2001.
[2] P. R. Roberge;R. D. Klassen;P. W. Haberecht .Atmospheric corrosivity modeling -- a review[J].Materials & Design,2002(3):321-330.
[3] Michael Zeigler .An overview of the wright laboratory structural integrity of aging aircraft core aera[R].AIAA Paper,1997.
[4] DANIEL J;GRONER P.E .US AIR FORCE AGING AIRCRAFT CORROSION[Z].AIAA,1997.
[5] 曹楚南.中国材料的自然环境腐蚀[M].北京:化学工业出版社,2005
[6] AILOR W H.Handbook on Corrosion Testing and Evaluation[M].New York:John Wiley and Sons,Inc,1971
[7] HOWARD J B;GILROY H M .Natural and Artifical Weathering of Polyethylene Plastics[J].Polymer Engineering and Science,1969,9(04):286-294.
[8] SIMMS J A .Accelerated shift factor and its use in evaluation weathering factor[J].Journal of Coatings Technology,1987,59(748):45-53.
[9] Peter Eriksson;Bo Carlsson;Inger Odnevall Wallinder .Design of accelerated corrosion tests for electronic components in automotive applications[J].IEEE transactions on components and packaging technologies: A publication of the IEEE Components, Packaging, and Manufacturing Technology Society,2001(1):99-107.
[10] ASTM G34-2001.ASTM G34-2001.Standard test method for exfoliation corrosion susceptibility in 2XXX and 7XXX series aluminum alloys (EXCO Test)[S].ASTM,2003.
[11] 陈群志 .腐蚀环境下飞机结构日历寿命技术体系研究[D].北京航空航天大学,1999.
[12] 曹楚南.腐蚀试验数据的统计分析[M].北京:化学工业出版社,1988
[13] 唐子龙 .孔蚀发展过程动力学分析[J].中国腐蚀与防护学报,1998,18(04):241-250.
[14] SHEIKH A K;BOOH J K;HANSEN D A .Statistical modeling of pitting corrosion and pipeline reliability[J].Corrosion,1990,36(03):190-197.
[15] 王松桂;陈敏;陈立萍.线性统计模型线性回归与方差分析[M].北京:高等教育出版社,1999
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