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 -> 高负荷叶型
1.
Study of High-loaded Blade Profile Design Method Based on Cylinder
基于圆柱面的高负荷叶型设计方法研究
2.
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
3.
Aerodynamic performance of a highly-loaded low-pressure turbine profile
一种大负荷低压涡轮叶型的气动性能
4.
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
5.
Demonstration is made by the case of Shanghai.
在模型中,高峰负荷被分解为3部分:居民空调负荷、作区空调负荷以及基本负荷。
6.
INVESTIGATION OF BOUNDARY LAYER DEVELOPMENT FOR DIFFERENT LOADING DISTRIBUTION CONSIDERING WAKE EFFECT
尾迹作用下不同负荷分布叶型边界层发展研究
7.
Large eddy simulation of separated flow transition on a highly-loaded low pressure turbine profile
大负荷低压涡轮叶型分离转捩流动的大涡模拟
8.
Gravity center modification method can be used in high-load rotor blade design in engineering.
重心线调节法可应用于高负荷叶片设计。
9.
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
10.
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
11.
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
12.
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
13.
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
14.
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
15.
The Application of Peak-load Pricing Model in Transport Industry;
高峰负荷定价模型在运输业中的应用
16.
Analysis on the Peak-load Pricing Model of China s Railway Passenger Transportation;
中国铁路客运高峰负荷定价模型分析
17.
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
18.
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