Effect of Nozzle Inlet Shape on Annular Swirling Flow with Non-Equilibrium Condensation

被引：0

作者：

Yusuke FUKUSHIMA ^{[1
]}

Shigeru MATSUO ^{[2
]}

Toshiaki SETOGUCHI ^{[3
]}

Norimasa SHIOMI ^{[4
]}

Tokitada HASHIMOTO ^{[2
]}

Heuy Dong KIM ^{[5
]}

and Shen YU ^{[6
]}

机构：

[1] Graduate School of Science & Engineering,Saga University

[2] Department of Advanced Technology Fusion,Saga University

[3] Institute of Ocean Energy,Saga University

[4] Department of Mechanical Engineering,Saga University

[5] School of Mechanical Engineering,Andong National University

[6] Institute of Engineering Thermophysics,Chinese Academy of Science

来源：

Journal of Thermal Science | 2015年 / 24卷 / 04期

关键词：

compressible flow; non-equilibrium condensation; supersonic annular nozzle; swirl flow; simulation;

D O I：

暂无

中图分类号：

O354.3 [超音速流动];

学科分类号：

摘要：

Recently,by combining a swirl flow with non-equilibrium condensation phenomena of condensate gas generated in a supersonic flow,a separating and extracting techniques of condensate gas have been developed.This technique can reduce the size of the device and don’t use chemicals.In the present study,by using a non-equilibrium condensation phenomenon of moist air occurred in the supersonic flow in the annular nozzle composed of an inher body and an outer nozzle with a swirl,the possibility of separation of the condensable gas and the effect of shape of nozzle inlet on the flow field were examined numerically.

引用

页码：344 / 349

页数：6

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