超声速气流中激波/边界层干扰微射流控制研究进展.
徐浩， 杜兆波， 钟翔宇， 黄伟 - Aero Weaponry, 2022 - search.ebscohost.com
激波/边界层干扰现象在超声速流场中不可避免, 这种现象的存在会对超声速飞行器内外流场
产生一系列的不利影响. 所以, 对激波/边界层干扰现象进行控制是十分必要的 …
产生一系列的不利影响. 所以, 对激波/边界层干扰现象进行控制是十分必要的 …
Control mechanism of vortex-generator jet on turbulent separation in a highly loaded compressor cascade
C Zhiyuan, S Cheng, G Wei… - Proceedings of the …, 2023 - journals.sagepub.com
The active flow control technique of vortex-generator jet (VGJ) was used to control the
turbulent separation of a highly loaded compressor cascade at a high incidence. VGJ …
turbulent separation of a highly loaded compressor cascade at a high incidence. VGJ …
[PDF][PDF] Control of shock-induced flow separation with Air-Jet vortex generators
DP Ramaswamy - 2023 - researchgate.net
Shock-wave/boundary-layer interactions (SWBLIs) are complex flowfields commonly
encountered in many high-speed aerospace applications. A strong shock wave imposes a …
encountered in many high-speed aerospace applications. A strong shock wave imposes a …