SAE ARP1795A – 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 tendency of pre-stressed titanium alloys to crack when subsequently heated to elevated temperatures.
Product Details
- Published:
- 10/01/1990
- File Size:
- 1 file , 440 KB
- Note:
- This product is unavailable in Ukraine, Russia, Belarus
