Prediction of Crack Initiation Life due to Corrosion Pits
Author:
Affiliation:
1. School of Mechanical and Power Engineering, East China University of Science and Technology, 200237 Shanghai, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C032436
Reference42 articles.
1. Corrosion fatigue on 2024T3 and 6056T4 aluminum alloys
2. Quantification of pitting in two tempers of 7075 aluminium alloy by non-destructive evaluation
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5. Comparative Study of Corrosion-Fatigue in Aircraft Materials
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