1) trailing edge blowing
尾缘喷气
1.
The investigation on trailing edge blowing on low-speed axial fan is studied in this paper.
尾缘喷气技术已经广泛地用于航空发动机和多级压缩机等领域,用以降低动静叶片间的相互干涉作用以提高透平机械的气动性能,并降低动静干涉噪声。
2) edge blowing mixture curtain(EBMC)
尾缘吹气
1.
An experimental study on initial spray field of edge blowing mixture curtain(EBMC) flame holder was conducted using a particle dynamics analyzer(PDA).
利用激光测雾仪(PDA)对尾缘吹气式火焰稳定器尾缘出口的初始雾化场进行了实验研究,在静止空气中测量了尾缘出口下游不同截面上的各点处的液滴直径、速度等参数,分析了雾化场结构,初步探讨了初始雾化场的特征。
3) edge blowing mixture curtain(EBMC) flame holder
尾缘吹气稳定器
4) trailing edge
尾缘
1.
The heat transfer and characteristics of the fluid flow in the duct with waist-shaped pin- fin arrays for the trailing edge of the turbine blade were experimentally investigated.
本文对涡轮叶片尾缘中具有束腰结构扰流柱的冷却通道的传热和流动阻力特性进行了实验研究,重点研究了雷诺数、扰流柱的束腰比以及不同组合的影响。
2.
Numerical methods are used to investigate the film cooling effect of turbine guide vane′s trailing edge.
采用数值模拟的方法,研究了涡轮叶片尾缘斜劈缝气膜冷却的流场特性,及其对叶背面尾缘温度分布的影响。
3.
In order to investigate the flow characteristics of cooling flow downstream of a turbine guide vane trailing edge slot,numerical methods of RNG k-ε turbulent model were solved.
通过RNG k-ε湍流模型求解可压流的N-S方程,研究燃气轮机涡轮导向叶片尾缘劈缝出流冷气的流动情况。
6) 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。
补充资料：缘气
【缘气】
（术语）缘虑心之气分也。(参见：缘影)
（术语）缘虑心之气分也。(参见：缘影)
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