| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 1502509 | Scripta Materialia | 2006 | 6 Pages |
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.
Related Topics
Physical Sciences and Engineering
Materials Science
Ceramics and Composites
Authors
Y.-C. Wang, A. Misra, R.G. Hoagland,