COMPARISON OF STRESS-CORROSION RESISTANCE OF BARE X2020-T6 SHEET AND BARE 7075-T6 SHEET
Abstract
End supported, centrally loaded, 0.063 in. x 1 in. x 9 in. beams of X 20 and 7075-T6 aluminum alloy sheet, held in an insulated clamping fixture were stressed to 80% of their ten tensile yield strength and exposed to salt spray atmosphere for 250 hours. At the end of the salt spray exposure no stress corrosion cracking was observed either in the X2020-T6 or 70 5-T6 alloy. During the salt spray corrosion exposure the X2020-T6 alloy pitted severely at the frequency of three to six 1/8 in. diameter by 1/16" deep pits per square inch. The 7075-T6 material did not pit as a result of salt spray corrosion exposure.
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 16, 1958
- Accession Number
- AD0292284
Entities
People
- E. C. Turner
- H. H. Stier
- P. W. Bergstedt
Organizations
- General Dynamics