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
收藏
页码：269 / 284
页数：16
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