Numerical prediction on the interaction between the incident shock wave and the transverse slot injection in supersonic flows
作者： Wei Huang , Zhen-guo Wang , Ji-ping Wu , Shi-bin Li
DOI: 10.1016/J.AST.2012.10.007
关键词:
摘要: Abstract The incident shock wave has a great impact on the transverse injection flow field in supersonic flows, and it can improve mixing efficiency between incoming fuel. In current study, interaction slot been investigated numerically, influences of size location ramp wall pressure profiles have performed. Additionally, swept angle is set to be 15.784°, 28.158° 35.974°, respectively. obtained results show that field, formed upstream moves towards entrance channel with increase jet-to-crossflow ratio. disturbed when at leading edge strong enough, separation regions both downstream intensity wave. large improvement
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