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.

引用

页数：5

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