1) leakage-vortex
泄漏涡带
2) tip leakage vortex
泄漏涡
1.
The measurement results indicated that a tip leakage vortex is produced very close to the le.
结果表明泄漏流在转子进口开始产生，泄漏涡约在１０％弦长最强，并迅速向压力面和低叶高方向移动，沿程造成高紊流和高阻滞。
3) leakage vortex
泄漏涡
1.
It is found that the propagation of tip leakage vortex produces a large blockage e.
数值分析峰值效率和失速边界工况下动叶和静叶间隙区域流动结构的变化表明:随着压气机的运行工况由峰值效率点向失速边界点移动,动、静叶间隙泄漏涡向下游发展过程中产生的阻塞效应明显增强,该阻塞效应是导致压气机失速的主要原因。
2.
The tip clearance leakage flow and leakage vortex were noticed in this numerical simulation.
该数值模拟捕捉到了叶顶间隙的泄漏流动及泄漏涡 ,得到了比较完整的能量特性图表并与实验数据吻合 。
3.
The details of the interaction between leakage flow and passage secondary flow and the details of generation and development of leakage vortex were predicted under different clearance scale and the condition of both stationary and rotating hub.
对于不同的间隙尺寸,对于环壁静止与旋转的不同壁面条件,揭示了泄漏流与通道二次涡相互作用的细节,揭示了泄漏涡的生成与发展过程。
4) tip leakage vortex
叶尖泄漏涡
1.
Based on the measurement results, this paper analyses the generation, evolution, unsteadiness and breaking of the tip leakage vortex of the compressor rotor at design condition and near stall conditions in detail.
基于瞬态场测量结果,详细分析了设计状态和近失速状态下压气机转子叶尖泄漏涡产生、发展、失稳、 破碎的演化过程。
2.
Three-dimensional flow of the tip leakage vortex inside an axial-flow compressor rotor passage was studied using a 3-D Laser Doppler Velocimetry.
小流量状态下叶尖泄漏涡产生于更靠近转子叶片前缘，旋涡强度大，发展迅速，在转子内距离前缘约２０％轴向弦长的截面达到最强，在８０％轴向弦长附近发生破裂。
5) tip leakage vortex
叶顶泄漏涡
6) scrapped tip leakage vortex
刮削泄漏涡
补充资料：板带轧制速度规程(见板带轧制规程设计)
板带轧制速度规程(见板带轧制规程设计)
speed schedule for plate and strip rolling
bandai zhazhi sudu guieheng板带轧制速度规程(speed seheduxe fo:plateand strip rolling)见板带札制规程设计。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条