作者: Y.-C. Wang , A. Misra , R.G. Hoagland
DOI: 10.1016/J.SCRIPTAMAT.2006.01.027
关键词: Order of magnitude 、 Composite material 、 Materials science 、 Composite laminates 、 Fatigue limit 、 Ultimate tensile strength 、 Layer thickness 、 Stress (mechanics) 、 Cavity magnetron 、 Nanoscopic scale
摘要: 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 magnitude increase in the stress failure was observed. The ratio fatigue endurance limit ultimate tensile strength about 0.35.