On sidewall boundary layer effects in two-dimensional subsonic and transonic wind tunnels

被引:0
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作者
Rasuo, B [1 ]
机构
[1] Univ Belgrade, Fac Mech Engn, YU-11000 Belgrade, Yugoslavia
关键词
D O I
暂无
中图分类号
O29 [应用数学];
学科分类号
070104 ;
摘要
In this paper a closed-form analysis of flow in a two-dimensional transonic wind tunnel that uses sidewall distributed suction around the model to reduce sidewall boundary-layer effects is presented.
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页码:S935 / S936
页数:2
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