基本释义:

正车叶片

网络释义

1)ahead blading,正车叶片

2)ahead blading,正车叶片组

3)positive curved blade,正弯叶片

4)pressure side of blade, face of blade,叶片正面

5)back blading,倒车叶片

6)centralizer lug,扶正器叶片

用法和例句

The flow fields were measured in the blade tip clearances of the cascade with the conventional straight and positive curved blade.

详细测量了常规直叶片与正弯叶片栅间隙内与上、下游流场，比较两套叶栅的实验结果发现：叶片正弯减小了叶顶后3／5轴向弦长范围内的横向压力梯度，并消除了上通道涡，因而大大削弱了泄漏流与瑞壁横流之间的相互干扰，相对漏气量与叶栅流动损失都显著降低。

Effect of Positive Curved Blade on Aerodynamic Performance of High-Turning Compressor Cascade;

正弯叶片对大折转角压气机叶栅气动性能的影响

Research on Cavitation is Restrained in Axial Water Pump by Crankle Blade;

叶片的弯扭对轴流泵汽蚀抑制的研究

The Research on the Inner Flow Characteristic of Circumferential Direction Bowed Blade with Mini Flow

小流量下周向弯曲叶片内流特性研究

Effects of swept-curved blade on the performance of the multistage fan

叶片弯掠对多级风扇气动性能的影响

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

Experimental study on the aerodynamic performance of aft-loading positive-curving blade

后加载正弯静叶栅气动性能试验研究

Numerical simulation of the aerodynamics performance of swept and curved blade on the compressor stator

叶片弯掠对压气机静子叶片气动性能影响的三维数值模拟

Effects of Circumferential Bowing Direction on the Aerodynamic and Acoustics Performance of the Bowed & Swept Blade Under Low Flow Rate Conditions

周向弯曲方向对弯掠叶片小流量工况下气动-声学性能的影响

Bend the bushing tabs so that they are contacting the leaf spring.

弯曲衬套接头以便接头能与叶片弹簧接触。

AEROELASTIC TAILORING FOR ROTOR BLADES OF TRANSONIC SWEPT FANS

跨音弯掠风扇转子叶片的气动弹性剪裁

Effect of circumferential forward-skewed blade on aeroacoustic performance of axial fan

周向前弯叶片对轴流风扇气动声学性能影响

Thermal analysis and design optimization for cooling passage of turbine blades

涡轮叶片转弯流道换热分析与优化设计

Investigation on Application of Dihedral/Swept Blade and Boundary Layer Suction to Control Vortex Configurations in Compressor Cascades;

采用叶片弯/掠及附面层抽吸控制扩压叶栅内涡结构的研究

Experimental and Numerical Investigation of Using Bowed Blade in Compressor Cascade with Different Turning Angles;

不同折转角压气机叶栅中应用弯曲叶片的实验与数值研究

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

Numerical analysis on tip leakage flow of circumferential skewed blades according to flow rates

周向弯曲叶片叶顶泄漏流随流量变化特性数值研究

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

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