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Author

Yong-Lei Qu

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Oct 2026

Vortex instability induced by blade-attached vortex generators in a supersonic compressor cascade under downstream throttling

The unsteady flow related to shockwave/boundary layer interaction is one of the key factors leading to compressor instability, so it is important to develop an effective flow control method. In this study, based on three-dimensional numerical simulation, the control mechanism of blade-attached vortex generator (BVG) on...

Tian-Chu Song, Zhong-Yi Wang, Hai-Meng Zhou et al. · 0 citations

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