1) blade wake
叶片尾迹
1.
A particle image velocimetry system was used to measure the secondary flow in the volute cross-section and the blade wake flow.
用粒子图像速度场仪技术对叶片尾迹区及蜗壳出口横截面上的二次流做了详细的变工况测量与分析。
2) non-reflecting
尾迹/叶片排干扰
3) impeller wakes
叶轮尾迹
4) turbine blade trailing edge
叶片尾缘
1.
Different structure diaphragm plates in complex passages of turbine blade trailing edge;
涡轮叶片尾缘复合通道隔板结构
2.
The experiment mainly aimed at to investigate the effect of different aperture in different clapboard structure in the turbine blade trailing edge complex passages on heat transfer and pressure drop characteristics.
采用热色液晶测温法,测量了涡轮叶片尾缘带隔板的复合通道的温度场。
5) trailing flow
叶片尾流
1.
The unsteady and viscous model based upon the weakly compressible flow has been established,Large Eddy Simulation(LES) approach is applied to simulating the mechanism of trailing flow of hydrofoils,and "partial-slip boundary condition " is developed for the solid wall boundary.
建立了基于弱可压缩流体基础之上的非恒定、粘性流数学模型,采用大涡模拟计算方法,固壁边界条件采用“部分滑移条件”,成功地对水力机械叶片尾流现象进行了模拟计算。
6) wake/blade interaction
尾迹/叶排干扰
补充资料：飞机尾迹
[[飞机尾迹]]：飞机飞行中发动机排出的废气与周围空气混合凝结而成的特殊的云。一般发生在气温低于-40度、又有适当湿度条件的空气层中。飞机尾迹对飞行没有影响，但暴露行踪，对航空兵战斗行动有一定的影响。
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