A numerical simulation is conducted with respect to an in－cascade flow field of a high－pressure turbine nozzle assembly of curved vanes in the case of the presence and absence of an air cooling spray.
对采用弯曲叶片的某型高压涡轮导向器有/无冷气喷射时的栅内流场进行了数值模拟。
High Pressure Nozzle Cascade of Steam Turbines Approaches to a Better Aerodynamic Performance
汽轮机高压级喷嘴叶栅气动性能改善的新途径
A Study on the Applicable Condition in the Transonic Cascade Calculation Using the Nozzle-Solution of the Mixed Equation in Hodograph
速度面混合型方程喷管解在跨音速透平叶栅计算中应用条件的研究
Design of multi-nozzle PM_ (10) - PM_ (2.5) cascade impactor and its application
多孔喷嘴PM（10）-PM（2.5）串级冲击式大气采样器的研制及应用
The nozzle cascade was designed for a Curtis stage using an advanced after-loaded flow control technique to reduce secondary flow losses.
该复速级喷嘴叶栅采用先进的后加载流动控制技术，以减弱叶栅的二次流损失。
Numerical Study of the Effect of Endwall Contouring on the Aerodynamic Performance of an Annular Nozzle Cascade
端壁收缩对环形叶栅气动性能影响的数值研究
To solve the problem of the flow in the nozzle cascade with many splitter vanes, this paper adopts the more advanced finite element method.
为了对这种多分流喷咀叶栅进行全流场计算，本文采用了较先进的气动变分有限元方法。