Influence of wind tunnel freestream turbulence level on boundary-layer separation

被引：0
|
作者：
I. D. Zverkov
V. V. Kozlov
A. V. Kryukov
机构：
[1] Khristianovich Institute of Theoretical and Applied Mechanics SB RAS,
[2] Novosibirsk State University,undefined
来源：
Thermophysics and Aeromechanics | 2011年 / 18卷
关键词：
wing stall; separation bubble; low Reynolds numbers; wing performance;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
An investigation of aerodynamic performance for micro air vehicle (MAV) wing is performed. It is shown, what is a reason of significant wing performance difference between tests, which were carried out in different wind tunnels. New method for estimation of wind tunnel condition influence on experimental results is suggested.
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页码：203 / 214
页数：11
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