Stress Corrosion Resistance of a New High Strength Aluminum Alloy Developed for Use in Thick Sections.
Abstract
The objective of the investigation was to evaluate the stress corrosion behavior of a new high strength aluminum alloy plate in the T6+35 hours at 325F temper. Using smooth specimens, stress corrosion tests were conducted in two different laboratory environments. No evidence of stress corrosion cracking was found in any of the test specimens. Exfoliation tests were also conducted on stepped panels which exposed different interior planes through the thickness. The material displayed excellent resistance to exfoliation corrosion. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 11, 1971
- Accession Number
- AD0734129
Entities
People
- Irving S. Shaffer
Organizations
- Naval Air Warfare Center Warminster