The results show that the shockwave structure is unsteady in shock induced hypersonic turbulent separated flows, generating an intermittent region.
结果表明：在激波诱导的高超音速湍流分离流中，激波结构是不稳定的，产生一个间歇区域。
2
It is shown by calculation and analysis that the main form of the interaction in compressor cascades is the interaction between shockwave and turbulent boundary layer 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。
3
Wall heat transfer fluctuations have been measured using a platinum film resistance thermometer in forward facing steps induced shockwave and turbulent boundary layer interaction fields.