compressor blade

Investigation on Simulation of foreign object impact damage to compressor blade

外物撞击损伤叶片的模拟试验方法

To investigate the forcing function effects on the fundamental 2 E gust unsteady aerodynamic response of a multistage turbomachine blade row, a series of fundamental experiments are performed in an axial flow research compressor.

为了研究扰动力函数对多级叶轮机叶片排中基本的高、低能阵发非定常气动响应的影响，在研究用轴流压气机上进行了一系列的基础研究。

The compressor blade leading edge flow is studied by hydrogen bubble flow visualization.

在水洞内使用氢气泡流动显示方法研究环绕压气机叶片前缘的流动.

Experimental investigation of surface static pressure in curved blade compressor cascade at different incidences

不同冲角下弯叶片扩压叶栅壁面静压的实验研究

Numerical optimization of compressor blade profile based on the control theory

基于控制理论的压气机叶型数值优化方法

An Experimental Investigation by Using Curved Blade in Compressor Cascades

环型扩压叶栅中应用弯曲叶片的研究

Influence of incidence on aerodynamic performance of compressor cascade with positive curved blade

冲角对正弯曲叶片扩压叶栅气动性能的影响

Ultrasonic testing of rotor blades in the high pressure compressor of aeroplane engine

飞机某型发动机高压压气机转子叶片的超声波检测

Breaking Reason Analysis for Axial-Centrifugal Compressor Blade

轴流-离心复合式压缩机叶片断裂原因分析

The tip leakage vortex is the main reason which causes tip gap leakage flow blockage and the turbulent flow in the blade tip gap of compressor.

叶尖泄漏涡是叶尖间隙气流流动阻塞和引起压气机转子尖部紊流脉动的主要因素。

Material Testing System and Application of Axial Compressor Blade

轴流压缩机叶片材料测试系统及应用