Abstract
Fatigue properties of magnetron sputtered Cu/Nb composite laminates with 40 nm individual layer thickness were determined. Compared to bulk Cu, over an order of magnitude increase in the stress to failure was observed. The ratio of the fatigue endurance limit to the ultimate tensile strength was about 0.35.
Original language | English |
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Pages (from-to) | 1593-1598 |
Number of pages | 6 |
Journal | Scripta Materialia |
Volume | 54 |
Issue number | 9 |
DOIs | |
Publication status | Published - 2006 May |
All Science Journal Classification (ASJC) codes
- General Materials Science
- Condensed Matter Physics
- Mechanics of Materials
- Mechanical Engineering
- Metals and Alloys