Exploring mechanism of stall margin enhancement of subsonic axial - flow compressor through steady micro tip injection 定常微量喷气提高轴流压气机稳定工作裕度机理探讨
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Analysis of the effect on tip flow topologies led to some preliminary conclusions as to the flow physics involved in the stall margin improvements afforded by tip injection 通过详细地分析顶部喷气对压气机顶部区域流场结构的影响，揭示了其扩稳机理。
