Numerical and experimental study of high-lift configurations

被引：1

作者：

Rumyantsev, A. G. ^{[1
]}

Silantiev, V. A. ^{[1
]}

机构：

[1] Chaplygin Siberian Res Inst Aviat SibNIA, Novosibirsk, Russia

来源：

THERMOPHYSICS AND AEROMECHANICS | 2010年 / 17卷 / 02期

关键词：

computation; experiment; Reynolds-averaged Navier - Stokes equations; Spalart - Allmaras one-equation turbulence model; high-lift configuration; low-speed wind tunnel;

D O I：

10.1134/S0869864310020125

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Flow of two high-lift devices is studied on the basis of the solution to two-dimensional Reynolds equations with the Spalart - Allmaras one-equation turbulence model. Computation results are compared with the experiment under the conditions of airfoil flow in the low-speed wind tunnel with open test section. It is shown that such approach is the most correct for this comparison.

引用

页码：269 / 284

页数：16

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