Large Eddy Simulation of an Asymmetric Jet in Crossflow

被引：6
|
作者：
Folkersma, M. [1 ]
Bodart, J. [1 ]
机构：
[1] Univ Toulouse, ISAE SUPAERO, Dept Aerodynam Energet & Prop, Toulouse, France
来源：
DIRECT AND LARGE-EDDY SIMULATION X | 2018年 / 24卷
关键词：
D O I：
10.1007/978-3-319-63212-4_10
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
On turbine blades, film cooling is an efficient way to prevent temperature to reach the blade material melting point, downstream the combustion chamber. Protection against continuous feeding of incoming hot gases is achieved by injecting coolant at the blade surface. To study turbulent mixing occurring in the jet vicinity we focus our attention on a jet in crossflow configuration. © 2018, Springer International Publishing AG.
引用
收藏
页码：85 / 91
页数：7
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