航空学报 > 1995, Vol. 16 Issue (3): 89-92

激波/边界层干扰脉动压力测量技术

张华, 邓学蓥   

  1. 北京航空航天大学流体力学研究所, 北京, 100083
  • 收稿日期:1993-12-20 修回日期:1994-04-28 出版日期:1995-06-25 发布日期:1995-06-25

THE FLUCTUATING WALL-PRESSURE MEASUREMENT IN SWEPT SHOCK WAVE/BOUNDARY LAYER INTERACTIONS

Zhang Hua, Deng Xueying   

  1. The Institute of Fluid Mechanics, Beijing University of Aeronautics and Astronautics, Beijing,100083
  • Received:1993-12-20 Revised:1994-04-28 Online:1995-06-25 Published:1995-06-25

摘要: 建立了激波/边界层干扰脉动压力测试系统。对一组后掠压缩角产生的激波/边界层干扰脉动压力流场进行测量,结果表明,脉动压力时均值及其分布与静态测量得到的结果一致。测量还发现在实验的锥形干扰范围内,未出现类似于二维干扰中由非定常低频振荡激波引起的间歇现象。

关键词: 激波, 边界层, 干扰, 压力振荡, 测量

Abstract: A fluctuating wall- pr essure measurement system is established. In a conical interactionflowfield produced by a set of swept compr ession corners, the measurement results show that the RMSvalue of fluctuating pressure and its distributions are consistent with those measured by static pressur emeasur ement system (with Scani probe) . The intermittent phenomenon caused by oscillat ing shockwave at relatively low frequencies did not appear obviously within the whole test region, which is dif2ferent from the r esults in two dimensional conditions.

Key words: shock waves, boundary layer, interfer ence, pressure oscillations, measurement

中图分类号: