OPTIMIZATION OF THE TANGENTIAL JET BLOWING ON A TRANSONIC AIRFOIL FOR BUFFET CONTROL

被引:0
|
作者
Abramova, K. A. [1 ]
Soudakov, V. G. [1 ]
机构
[1] Zhukovsky Cent Aerohydrodynam Inst, Zhukovskii, Russia
基金
俄罗斯科学基金会;
关键词
wing airfoil; shock-boundary layer interaction; boundary layer; tangential jet blowing; numerical simulation; optimization; SHOCK CONTROL;
D O I
10.1134/S0021894424020020
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
AbstractOptimization of tangential jet blowing on the upper surface of a supercritical transonic airfoil under buffet conditions was carried out. Two-dimensional unsteady Reynolds-averaged Navier-Stokes equations were solved to simulate the flow past the airfoil. The Spalart-Allmaras turbulence model was used to close the equations. The location of the slot nozzle and the intensity of the jet blowing from it were varied. The optimal location for blowing with minimum jet intensity to suppress buffet was determined.
引用
收藏
页码:202 / 209
页数:8
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