Article ID Journal Published Year Pages File Type
7048816 Applied Thermal Engineering 2015 8 Pages PDF
Abstract
Flow distribution for the aviation kerosene in parallel helical tubes under the supercritical pressure of 3 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
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