Experimental and theoretical investigation of boundary layer perturbations on a low-aspect-ratio wing

被引：0
|
作者：
Kozlov V.V. [1 ]
Zverkov I.D. [1 ]
Zanin B.Yu. [1 ]
Dovgal A.V. [1 ]
Rudyak V.Ya. [2 ,3 ]
Bord E.G. [2 ]
Kranchev D.F. [2 ,3 ]
机构：
[1] Khristianovich Institute of Theoretical and Applied Mechanics, SB RAS, Novosibirsk
[2] Novosibirsk State University of Architecture and Civil Engineering, Novosibirsk
[3] Novosibirsk State Technical University, Novosibirsk
来源：
Thermophysics and Aeromechanics | 2006年 / 13卷 / 4期
基金：
俄罗斯基础研究基金会;
关键词：
Wind Tunnel; Separation Bubble; Laminar Boundary Layer; Instability Wave; Wing Surface;
D O I：
10.1134/S0869864306040044
中图分类号：
学科分类号：
摘要：
Laminar-turbulent transition in a boundary layer of low-aspect-ratio wing was investigated. Experiments clarifying the flow structure, its mean and oscillatory characteristics were carried out accompanied by linear stability analysis of the wind tunnel data on the laminar flow velocity profiles. Theoretical results obtained in a parallel flow approximation are in a good agreement with the experimental data on disturbances evolution at the initial stage of transition to turbulence.
引用
收藏
页码：507 / 514
页数：7
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