Fatigue Life Model for 7050 Chromic Anodized Aluminium Alloy
Author:
Publisher
Elsevier BV
Subject
Applied Mathematics
Reference31 articles.
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2. On fatigue crack initiation from corrosion pits in 7075-T7351 aluminium alloy;Pao;Scripta Materialia,1998
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1. Chromium/nickel-free conversion coating as cold post-treatment to anodized AA2024-T3 for corrosion resistance increase;Surface and Coatings Technology;2024-03
2. The role of peening processes as a pre‐treatment to anodizing on fatigue behavior of aircraft aluminum alloy;Fatigue & Fracture of Engineering Materials & Structures;2024-01-25
3. A historical, statistical and electrochemical approach on the effect of microstructure in the anodizing of Al alloys: a review;Critical Reviews in Solid State and Materials Sciences;2023-07-09
4. Effect of end milling, grinding and tartaric-sulfuric anodizing on the fatigue behavior of AA7050 alloy;The International Journal of Advanced Manufacturing Technology;2022-09-17
5. Aluminum ASA 6061 Anodizing Process by Chromic Acid Using Box–Wilson Central Composite Design: Optimization and Corrosion Tendency;Metals and Materials International;2020-06-06
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