1.
EFFECTS OF BOUNDARY LAYER SUCTION ON THE LOSS OF HIGHLY-LOADED COMPRESSOR CASCADE
附面层抽吸对高负荷扩压叶栅损失的影响
2.
Effects of Blowing Location on Highly-Loaded Compressor Cascade Performance
吹气位置对高负荷扩压叶栅性能的影响
3.
EFFECTS OF BOUNDARY LAYER SUCTION ON THE FLOW AND LOAD OF HIGHLY-LOADED COMPRESSOR CASCADE
附面层抽吸对高负荷扩压叶栅流动及负荷的影响
4.
Experimental investigation on the span loading in compound lean compressor cascades with slots air injection
高负荷缝隙弯曲扩压叶栅展向负荷实验
5.
Experiment on wake characteristics in compound lean compressor cascades with slots injection
高负荷缝隙弯曲扩压叶栅尾迹特性实验
6.
Effect of Boundary Layer Suction on the Performance in a Highly-Loaded Compressor Cascade
高负荷压气机叶栅采用附面层抽吸的实验研究
7.
Effects of boundary layer suction on the flow fields of highly-loaded compressor cascades
附面层抽吸对高负荷压气机叶栅流场的影响
8.
Analysis of the Aerodynamic Performance of a Super-highly Loaded Adsorption Type Compressor Cascade
超高负荷吸附式压气机叶栅气动性能分析
9.
Enhancing Aerodynamic Performances of Highly Loaded Compressor Cascades via Air Injection
孔隙射流对高负荷压气机叶栅气动性能影响的实验研究(英文)
10.
Analysis of the Mechanism Governing the Migration of Boundary Layers in a Highly-loaded Turbine Cascade Controlled By Using Bowed Blades
采用弯叶片控制高负荷涡轮叶栅内附面层迁移的机理分析
11.
A NUMERICAL INVESTIGATION OF APPLICATION OF BOWED BLADE TO CONTROL FLOW SEPARATION ON HIGHLY LOADED TURBINE CASCADES
在高负荷涡轮叶栅中应用弯叶片控制流动分离的实验研究
12.
The Investigation of Vortex Structure in Straight and Compound Lean Compressor Cascades Via PIV;
直弯扩压叶栅内旋涡结构PIV研究
13.
An Experimental Investigation by Using Curved Blade to Control Secondary Flow in Compressor Cascade;
弯曲叶片控制扩压叶栅二次流动的实验研究
14.
Numerical Simulation and Control of Separated Transition Flows in High-lift Low-pressure Gas Turbine Cascade
低压高负荷燃气透平叶片边界层分离转捩数值模拟与流动控制
15.
An Investigation of Vortex Structure in High-Turning Dihedral Compressor Cascade with PIV;
大转折角弯曲扩压叶栅旋涡结构PIV研究
16.
The Aerodynamic/Structure Design of Subsonic Aspirated Compressor Cascade;
亚声速附面层抽吸式扩压叶栅气动/结构设计
17.
The Experimental Research on the Tangent Slot Injection Flow to the Performance of Diffusion Cascades;
切向孔隙改善扩压叶栅性能的实验研究
18.
Effects of air injection on outlet flow field of compressor cascade
孔隙射流结构对扩压叶栅出口流场特性的影响