Separation characteristics and competitive mechanism of corner separation and mid-span separation in a high-speed compressor cascade at low Reynolds numbers

分离(统计) 流动分离 雷诺数 机械 层流 气泡 唤醒 气体压缩机 边界层 级联 材料科学 流量(数学) 涡流 物理 分离过程 轴流压缩机 阻塞流 攻角 失速(流体力学) 分离原理 大涡模拟 入口
作者
Qiang Liu,Peiqiang LU,Chongshan Liu,Dingxi Wang
出处
期刊:Chinese Journal of Aeronautics [Elsevier BV]
卷期号:: 104296-104296
标识
DOI:10.1016/j.cja.2026.104296
摘要

Under low-Reynolds-number ( Re ) conditions, compressor performance deteriorates markedly due to complex boundary layer separation phenomena. While both corner separation and mid-span separation bubble are known sources of loss, their interaction, particularly how they compete or merge under low- Re flows, remains poorly characterized. To unravel their unsteady interaction, this study employs Large Eddy Simulation (LES) to investigate the influence of low- Re on mid-span separation and corner separation in a high-speed compressor cascade. LES predictions, validated against experimental data, accurately capture the complex three-dimensional flow within the corner region. The analysis reveals two critical Reynolds numbers governing distinct flow regimes. Below Critical Re 1 (1.5 × 10 5 -1.8 × 10 5 ), the mid-span laminar separation bubble bursts into open separation, triggering rapid boundary-layer thickening and wake expansion, resulting in a surge in loss, while corner separation is suppressed and merges with mid-span separation. Above Critical Re 2 (around 2.0 × 10 5 -2.5 × 10 5 ), the mid-span outlet flow angle exhibits a negligible increase as Re decreases. However, between Critical Re 1 and Critical Re 2 , the rate of increase sharpens significantly. In contrast, the corner region shows an opposing flow angle response. Moreover, as Re decreases to below Critical Re 2 , the dominant loss shifts from corner separation to profile loss. A competitive mechanism between mid-span separation and corner separation, driven by the corner cross-flow, is also uncovered. Below Critical Re 2 , this crossflow intensifies mid-span transition, promotes spanwise redistribution of disturbance energy, and alters the total pressure loss distribution. The revealed competitive mechanism and the critical Reynolds numbers identified in this study form a crucial foundation for designing compressor aerodynamics that can control separation and minimize losses under challenging low- Re conditions.

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