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

查看全文 作  者:Yusuke [1]FUKUSHIMA;Shigeru [2]MATSUO;Toshiaki [3]SETOGUCHI;Norimasa [4]SHIOMI;Tokitada [2]HASHIMOTO;Heuy Dong [5]KIM;and Shen [6]YU 高影响力作者 机构地区:[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高影响力机构 出  处:《Journal of Thermal Science》索引2015年第24卷第4期,共6页高影响力期刊 基  金:supported by JSPS KAKENHI Grand number 26420116 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. 关 键 词:环形喷嘴 非平衡态 旋转流动 形状 入口 超音速流动 冷凝 提取技术
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