It is shown by calculation and analysis that the main form of the interaction in compressor cascades is the interaction between shockwave and turbulent boundarylayer in channels.
作者经过计算和分析，说明压气机叶栅流中主要的相互作用形式是叶栅槽道中激波和湍流附面层的相互作用。
2
Wall heat transfer fluctuations have been measured using a platinum film resistance thermometer in forward facing steps induced shockwave and turbulent boundarylayerinteraction fields.
用铂膜电阻温度计测量了前向台阶诱导激波与湍流边界层相互作用流场中的表面热流率脉动。
3
However, no thorough investigation has been made on shockwaveboundarylayerinteraction in compressor cascades and only a few papers on this topic have been published.