Film cooling effectiveness with injection through circular holes embedded in a transverse trench

被引:17
|
作者
Pakhomov, M. A. [1 ,2 ]
Terekhov, V. I. [1 ]
Khalatov, A. A. [3 ]
Borisov, I. I. [3 ]
机构
[1] RAS, SB, Kutateladze Inst Thermophys, Novosibirsk, Russia
[2] Tomsk State Univ, Tomsk 634050, Russia
[3] NAS Ukraine, Inst Engn Thermophys, Kiev, Ukraine
基金
俄罗斯基础研究基金会;
关键词
film cooling; thermal effectiveness; gas screen; blowing through holes; trench; numerical calculations; HEAT-TRANSFER; FLOW;
D O I
10.1134/S0869864315030075
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Results of a numerical study of the thermal effectiveness of a gas wall screen implemented via gas blowing through cylindrical inclined holes embedded in a transverse trench are reported. The calculations were performed using 3D Reynolds-averaged Navier-Stokes equations, with the flow turbulence being modeled by means of the Reynolds-stress model. Blowing into the trench was compared to the conventional cooling technique using gas blowing without a trench. The film cooling effectiveness with gas injection through circular holes embedded in trench exceeds significantly the effectiveness of blowing without a trench. Such a method of coolant supply into the flow proved to be especially advantageous at high blowing ratios. Due to the formation of vortical structures inside the trench, a more uniform cooling flow in the spanwise direction can be achieved. A comparative analysis is indicative of acceptable qualitative agreement of the experimental and predicted data.
引用
收藏
页码:329 / 338
页数:10
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