Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
7048816 | Applied Thermal Engineering | 2015 | 8 Pages |
Abstract
Flow distribution for the aviation kerosene in parallel helical tubes under the supercritical pressure of 3Â MPa. The helical tube has the curvature ratio of 0.06. It can be seen that significant flow mal-distribution generates at the critical point and flow distribution shows various results under different physical factors.
Related Topics
Physical Sciences and Engineering
Chemical Engineering
Fluid Flow and Transfer Processes
Authors
Yanchen Fu, Zhi Tao, Guoqiang Xu, Hongwu Deng, Zhouxia Jia,