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 -> 跨音速叶栅
1.
Numerical Simulation of the Aerodynamic Performance of the Improved Compressor Blade
叶型改型对压气机跨音速叶栅气动性能影响的研究
2.
Numeric Investigation of Using Endwall Fences in Annual Cascade of Transonic Compressor;
跨音速环形压气机叶栅中应用翼刀技术的数值研究
3.
Numerical Research on Effects of Splitter Blades on a Transonic Centrifugal Compressor Impeller
跨音速离心压缩机叶轮分流叶片的数值研究
4.
CALCULATION OF UNSTEADY AERODYNAMIC FORCE CAUSED BY OSCILLATION OF SUPERSONIC CASCADE
超音速叶栅由于振动引起的非定常空气动力的计算
5.
Numerical Simulation of Shock Waves and Interaction of Shock and Boundary Layer Within Supersonic Cascade;
超音速叶栅内的激波系及其与附面层相互作用的数值研究
6.
trisonic aerodynamics
三音速(亚音速、跨音速 、超音速)空气动力学
7.
Analysis of the Influence of the Aspect Ratio of a Transonic Compressor on the Aerodynamic Performance of Bowed and Swept Blades
跨音速压气机中展弦比对弯掠叶片气动性能影响的分析
8.
NUMERICAL SIMULATION ON UNSTEADY TIP LEAKGAE FLOW IN A TRANSONIC AXIAL FAN ROTOR
某跨音速轴流压气机转子叶顶泄漏流的非定常特征
9.
transsuper aerodynamics
跨音速和超音速空气动力学
10.
Intelligent Control of Speed and Position in the Dynamic Multi-leaf Collimator;
电动多叶光栅叶片位置和速度的智能控制
11.
high-solidity cascade
大调度叶栅, 稠叶栅
12.
UNSTEADY RESPONSE OF TIP LEAKAGE FLOW TO DISCRETE MICRO TIP INJECTION IN A TRANSONIC AXIAL COMPRESSOR AND ITS EFFECT ON STABILITY ENHANCEMENT
跨音速轴流压气机叶顶间隙泄漏流对微喷气的非定常响应机制和扩稳效果研究
13.
Numerical Investigation on the flow in a stage of Transonic Centrifugal Compressor with Vaned Diffuser Coupling with Different Configuration of Volute
单级跨音速离心压缩机叶片扩压器和不同蜗壳形式耦合的内部流动数值研究
14.
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
15.
A numerical study of unstalled two dimentional flow on an oscillating cascade
非失速二维振荡叶栅非定常流动数值模拟研究
16.
Stability of Transonic Shocks in Supersonic Flow Past a Wedge;
超音速绕流中产生的跨音速激波的稳定性研究
17.
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。
18.
Empirical results are needed in the transonic Mach regime.
在跨音速马赫数范围内需要经验结果。