leakage-vortex 泄漏涡带
Tip leakage vortex 顶部间隙泄漏涡
rotor tip leakage vortex 转子叶尖泄漏涡
scrapped tip leakage vortex 刮削泄漏涡
center of tip leakage vortex 叶顶泄漏涡涡心
NASA-37 transonic and NWPU-1 subsonic rotors are calculated by using this program. Results of calculation indicates that this program can admirably simulate rotor rows flow in axial compressors and distinguish passage shock, leakage vortex path and separation of boundary layer.
用该程序分别计算了NASA-37跨音速转子和NWPU-1亚音速转子，计算结果表明本文建立的孤立转子程序能够较好的模拟轴流压气机叶片排内流动情况，能够有效的捕捉通道激波和间隙泄漏涡轨迹以及叶片附面层的分离。
参考来源 - 轴流压气机叶顶间隙流动研究·2,447,543篇论文数据，部分数据来源于NoteExpress
The rotor tip leakage vortex has a stronger influence on the downstream endwall flow than the rotor wake.
同转子尾迹相比，转子叶尖泄漏涡对静子尖区的影响更为明显和深远。
The tip leakage vortex may have greater effect than other vortexes, that is consistent with the experimental results.
不同二次流与叶片颤振的相关性中尖部漏流涡对叶片气弹稳定性的影响较大。
The radial component is the highest of the three turbulence intensities in the corner vortex or leakage vortex region.
角区旋涡及泄漏涡影响区域紊流强度较高，其中径向分量最高，远大于轴向和切向分量。
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