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Stress Corrosion of Titanium Alloys, Effect of Cleaning Agents on Aircraft Engine Materials
This document establishes a test procedure for determining the propensity of aircraft turbine engine cleaning and maintenance materials for causing stress-corrosion cracking of titanium alloy parts.
The evaluation is conducted on representative titanium alloys by determining the effect of contact with cleaning and maintenance materials on the tendency of pre-stressed titanium alloys to crack when subsequently heated to elevated temperatures.
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