Fatigue Crack Origins in 7075-T6 and 7079-T6 Aluminum Alloys
Fatigue Crack Origins in 7075-T6 and 7079-T6 Aluminum Alloys
Author | Search for: 1; Search for: 1; Search for: 1 |
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Affiliation |
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Format | Text, Article |
Conference | 16th Aerospace Structures and Materials Symposium, Canadian Aeronautics and Space Institute (CASI), From 4/28/2003 To 4/30/2003., Montreal, Canada |
Subject | Fatigue; Aluminum alloys; Nucleation; Anodizing; Crack origin |
Access condition |
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Peer reviewed | Yes |
NRC number | SMPL-2003-0015 |
NPARC number | 8926697 |
Export citation | Export as RIS |
Report a correction | Report a correction (opens in a new tab) |
Record identifier | d8796e75-07d9-43b5-924e-ebdd354448d5 |
Record created | 2009-04-23 |
Record modified | 2020-04-16 |
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