Analysis and modeling of a two-phase jet pump of a thermal management system for aerospace applications

被引:42
作者
Sherif, SA
Lear, WE
Steadham, JM
Hunt, PL
Holladay, JB
机构
[1] Univ Florida, Dept Mech Engn, Gainesville, FL 32611 USA
[2] NASA, George C Marshall Space Flight Ctr, Thermal & Life Support Div, Huntsville, AL 35812 USA
关键词
jet pumps; ejectors; two-phase flow; aerospace thermal management;
D O I
10.1016/S0020-7403(98)00123-4
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Jet pumps are devices capable of pumping fluids to a higher pressure by inducing the motion of a secondary fluid employing a high-speed primary fluid. The main components of a jet pump are a primary nozzle, secondary fluid injectors, a mixing chamber, a throat, and a diffuser. The work described in this paper models the flow of a two-phase primary fluid inducing a secondary liquid (saturated or subcooled) injected into the jet pump mixing chamber. The model is capable of accounting for phase transformations due to compression, expansion, and mixing. The model is also capable of incorporating the effects of the temperature and pressure dependency in the analysis. The approach adopted utilizes an isentropic constant-pressure mixing in the mixing chamber and at times employs iterative techniques to determine the flow conditions in the different parts of the jet pump. (C) 1999 Elsevier Science Ltd. All rights reserved.
引用
收藏
页码:185 / 198
页数:14
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