本文采用数值方法模拟了一个三孔探头周围与测压孔内的二维可压缩非定常流场,研究了动态效应对探头绕流和测孔压力的影响以及相应的测量误差.结果显示当流场高频振荡时 (如:2000 Hz),其有效测量范围内的速度误差为2-4%,气流角误差约为l0%之内.当流动接近失速时,该项误差迅速增大.文中还给出了高频振荡流中测压孔内外非定常与准定常流场分布之间的差异.
参考文献
[1] | Bohn D;Schnittfeld T H.The Dynamic Response of Capillary Tubes for Use in Miniature Pressure Probes[A].Germany,1992 |
[2] | Kovasznay L S G;Tani I;Kanamura M et al.Instantaneous Pressure Distribution around A Sphere in Unsteady Flow[J].Journal of Fluids Engineering,Transactions of the ASME,1981,103:497-502. |
[3] | Humm Hans;Gossiveiler Christoph;Gyarmathy George .On Fast-Response Probes: Part 2-Aerodynamic Probe Design Studies[R].94-GT-27 |
[4] | Bohn D;Li Y;Schnittfeld T H.A Numerical Investigation of The Flow Around Probe Heads at Different Reynolds Numbers and Much Numbers[A].北京,1994:430-435. |
上一张
下一张
上一张
下一张
计量
- 下载量()
- 访问量()
文章评分
- 您的评分:
-
10%
-
20%
-
30%
-
40%
-
50%