Numerical Simulation of the Flow around the Wing in Takeoff-Landing Configuration

被引：0
|
作者：
Bosnyakov, S. M. [1 ]
Mikhaylov, S. V. [1 ]
Vlasenko, V. V. [1 ]
机构：
[1] Cent Aerohydrodynam Inst TsAGI, Zhukovsky Str 1, Zhukovskii 140185, Moscow Region, Russia
来源：
INTERNATIONAL CONFERENCE ON THE METHODS OF AEROPHYSICAL RESEARCH (ICMAR 2018) | 2018年 / 2027卷
基金：
俄罗斯基础研究基金会;
关键词：
D O I：
10.1063/1.5065143
中图分类号：
TH [机械、仪表工业];
学科分类号：
0802 ;
摘要：
Two series of calculations are presented. The first one is a separated flow in vicinity of airfoil in high-lift configuration. The second one is the same flow over 3D high-lift wing. All CFD data arc compared with experimental results. Physical phenomena are discussed. It is shown that the separated zones impact flowfield essentially.
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页数：5
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