What is it about?
The Aluminum (Al)- Magnesium (Mg) 5000-series alloys are currently used on Naval warships to reduce weight while also maintaining a high structural strength, which enables more fuel efficiency and faster travel. However, these alloys are utilized with different Mg contents, such as ~ 5 wt. % in AA5083 and ~5.5 wt. % Mg in AA5456, as well as with different heat treatments. The problem is, these alloys undergo intergranular stress corrosion cracking (IG-SCC) with time in service, and the effects of these different Mg percentages and different heat treatments on the severity of IG-SCC is not fully understood. Therefore, this work is a comparative study to show the effect of increased Mg content, as well as the effect of different treatments, on the eventual IG-SCC behavior to better understand which alloys are more advantageous for future use.
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Why is it important?
The impact of this paper lies primarily in the fact that: 1) A hydrogen-based failure model is successfully utilized to explain effects related to heat treatment and composition on the IG-SCC severity demonstrated experimentally 2) The alloy AA5456-H116 is, on average, shown to be less susceptible to IG-SCC than AA5083-H116 3) The Nitric Acid Mass Loss Test, which is used by the Navy and in research to estimate an alloy's IG-SCC susceptibility after time in service, is called into question by evidence of significant differences in nitric acid corrosion morphology between different heat treatments
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This page is a summary of: The Effect of Temper and Composition on the Stress Corrosion Cracking of Al-Mg Alloys
, CORROSION, December 2016, NACE International,
DOI: 10.5006/2317.
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