The Corrosion Morphology and Crack Growth Analysis of Aluminum Alloy

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Abstract:

The relation between corrosion depth and width with corrosion time is according with the power function. The corrosion pits can be seen as ellipse balls through the examination of QUESTAR three-dimensional optics microscope. Corrosion can decrease the fatigue life of materials and is the main reason of fatigue crack form and grow; through AFGROW analyze we can see that the AFGROW software can simulate crack growth life well and the error is low, the crack growth life and critical crack length are conservative than experiment values.

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464-468

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July 2011

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© 2011 Trans Tech Publications Ltd. All Rights Reserved

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[1] Jiuyuan Zhang.The comparison statistical law of pitting corrosion. [J].Chinese Society for Corrosion and Protection, 1994, Vol. 8(2).

Google Scholar

[2] Cunan Cao.Statistical analysis of corrosion test data [M]. Beijing: Chemical Industry Press, (1988).

Google Scholar

[3] Zhizong Mu.Reliability model and Application of Corrosion. 1999Reliability Engineering Society of China, 1999. 3.

Google Scholar

[4] He Ren.Corrosion model and reliability analysis of yun7aircraft [J]. Corrosion Science and Protection Technology, 1998, Vol. 10(4).

Google Scholar

[5] Zhentong Gao,Fatigue Applied Statistics [M]. Beijing: National Defence Industry Press, (1986).

Google Scholar

[6] Xianchao Hao,Xiaogang Lin,Chaofang Dong.Exposure time under different atmospheric corrosion of stainless steel in a typical Gray Analysis [J]. Corrosion Science and Protection Technology, 2008:30(5):503-504.

Google Scholar

[7] Hezhong Pei, Qilong Yong, Lei Jin. Atmospheric corrosion of metallic materials and environmental factors Grey Relational Analysis [J]. Iron and Steel Research, 1999: 11(4):53-54.

Google Scholar

[8] Sifeng Liu, Yaoguo Dang, Zhigeng Fang. Grey system theory and its application [M]. Beijing: Science Press, 2008: 50-96.

Google Scholar

[9] Zuotao Zhu, Zhitao Mu, Dinghai Chen. Research on evaluation of corrosion grade based on image processing technique [A]. 2009international Conference on Manufacturing Science and Engineering. 2009: 178-184.

Google Scholar

[10] Manning S D, Yang J N. Guidelines for analysis and design of durable aircraft structures. USAF Durability Design Handbook, AD-A 142424, (1984).

DOI: 10.21236/ada142424

Google Scholar

[11] Itzhak, D. Dinstein, I & Zilberberg, T. Pitting corrosion evaluation by computer image processing [J]. Corrosion Science, 1981, 21(1): 17-22.

DOI: 10.1016/0010-938x(81)90059-7

Google Scholar

[12] Wanhill R J H, Luceia J J De, RusslM T. The fatigue in aircraft corrosion testing programme. AGARD report No713, Feb, (1989).

Google Scholar