说明:双击或选中下面任意单词,将显示该词的音标、读音、翻译等;选中中文或多个词,将显示翻译。
您的位置:首页 -> 句库 -> 涡轮叶栅
1.
Effects of leading-edge modification on secondary flow in turbine cascades
叶片前缘改型对涡轮叶栅二次流的影响
2.
Research on the Heat Transfer of the Endwall Film-cooling in Axial Flow Turbine Cascade;
轴流涡轮叶栅端壁气膜冷却的传热研究
3.
Numerical Study of the Augmented Cooling on the Trailing Edge of Turbine Blade;
涡轮叶栅尾缘强化冷却方法的数值研究
4.
Effect of different incidences on turbine cascades flow in blade tip clearance
冲角变化对涡轮叶栅内间隙流动的影响
5.
Numerical Investigation of Air-cooled Gas Turbine Flow and Thermal Stress Characteristics
气冷涡轮叶栅流动及热应力特性的数值研究
6.
Experiment on flow control using Gurney-flaps for a low-pressure turbine cascade
基于Gurney襟翼的低压涡轮叶栅流动控制实验
7.
THE INVESTIGATION FOR INFLUENCE OF WAKE ON SECONDARY FLOW IN A TURBINE CASCADE
涡轮叶栅尾迹对二次流影响的试验研究
8.
Optimization Design on Tangential Stacking Law of Gas Turbine Cascade
燃气涡轮叶栅的周向积叠规律优化设计
9.
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
10.
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
11.
Experimental Investigation of the Aerodynamic Performance of Bowed Blades in High-turning Linear Turbine Cascades
弯叶片对大转角平面涡轮叶栅气动性能影响的实验研究
12.
Influence of Axially-swept Blades on the Aerodynamic Performance of a Turbine Stationary Cascade
轴向掠对涡轮静叶栅气动性能的影响
13.
THE EXPERIMENTS FOR GASTURBINE PLANE CASCADE IN A SHOCK TUNNEL
在激波风洞中进行的涡轮平面叶栅实验
14.
Study on the Turbine Stator Secondary Flow Using Moving Cylinders to Simulate Rotating Blades
采用运动圆柱模拟动叶的涡轮静叶栅二次流研究(英文)
15.
Numerical simulation on three-dimensional turbulent flow in a exhaust gas turbine stage cascade for supercharged marine boiler
船用增压锅炉烟气涡轮级叶栅三维湍流流动的数值模拟
16.
Flow Field Characteristics of Stator Cascade with Extremely Low Aspect Ratio in an Ultra-micro Gas Turbine
超微型涡轮中极低展弦比静叶栅流场特性的数值研究
17.
conduction-cooled turbine blade
(导热)冷却式涡轮叶片
18.
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