High Strain Rate Compressive Characterization of Aluminum Alloy/Fly Ash Cenosphere Composites

被引:42
作者
Luong, Dung D. [1 ]
Gupta, Nikhil [1 ]
Daoud, Atef [2 ]
Rohatgi, Pradeep K. [3 ]
机构
[1] NYU, Polytech Inst, Dept Mech & Aerosp Engn, Composite Mat & Mech Lab, Brooklyn, NY 11201 USA
[2] Helwan, Cent Met Res & Dev Lab, Cairo, Egypt
[3] Univ Wisconsin, UWM Ctr Composites & Adv Mat Manufacture, Dept Mat Engn, Milwaukee, WI 53201 USA
基金
美国国家科学基金会;
关键词
PRESSURE INFILTRATION TECHNIQUE; FLY-ASH; SYNTACTIC FOAMS; MECHANICAL-PROPERTIES; PARTICLES; BEHAVIOR; DAMAGE;
D O I
10.1007/s11837-011-0029-y
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The strain rate dependence of compressive response is determined for aluminum alloy/hollow fly ash cenosphere composites. A4032 alloy is used as the matrix material. Quasi-static and high strain rate compression tests are conducted on the matrix alloy and the composite. A split-Hopkinson pressure bar is used for high strain rate testing. While the matrix alloy does not show any appreciable strain rate sensitivity, the composite shows higher strength at higher strain rates. The energy absorption capability of A4032/fly ash cenosphere composites is found to be higher at higher strain rates.
引用
收藏
页码:53 / 56
页数:4
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