摘要
在小型风洞上，测量了叉排型扰流柱排内部的流场分布，得到了叉排型扰流柱排内部流场速度、旋涡和压力的详细分布情况，发现奇数和偶数测量截面上的速度分布规律不同，在奇数截面上可以观察到通道涡。
An experimental study was performed to investigate the staggered pin fin array flow field in the specially constructed small wind tunnel.The experimental result gives the detailed distributions of the flow field parameters.The analysis reveals that the velocity distribution on the odd measuring plane is different from that on the even measuring plane.Channel vortex can be observed on the odd measuring plane,and horseshoe vortex is caughted on the even measuring plane.
出处
《航空动力学报》
EI
CAS
CSCD
北大核心
1997年第2期175-179,共5页
Journal of Aerospace Power
关键词
扰流器
涡
流场
Spoilers Vortex Flow fields
