Experimental investigation on the stall process of a transonic compressor rotor

WANG Zhuo-qi; YUAN Wei; SONG Xi-zhen; LI Mao-yi; LU Ya-jun

Chinese

您当前的位置：

首页 >

文章列表页 >

Experimental investigation on the stall process of a transonic compressor rotor

更新时间：2026-07-07

- Experimental investigation on the stall process of a transonic compressor rotor
- Vol. 27, Issue 7, (2012)
- 作者机构：
  
  北京航空航天大学能源与动力工程学院航空发动机气动热力国家级重点实验室,北京,100191
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2012
- 稿件说明：
移动端阅览
WANG Zhuo-qi, YUAN Wei, SONG Xi-zhen, et al. Experimental investigation on the stall process of a transonic compressor rotor[J]. 2012, 27(7).
DOI：

WANG Zhuo-qi, YUAN Wei, SONG Xi-zhen, et al. Experimental investigation on the stall process of a transonic compressor rotor[J]. 2012, 27(7). DOI：

摘要

针对一台跨声速压气机转子在不同转速下的失速过程进行了稳态和动态实验研究.通过对原始信号、小波分析结果以及FFT(fast Fourier transform)变换结果的分析得到

该压气机转子在3个不同转速时均为突跃型全叶高失速

流场中存在一个失速团

失速团沿周向的传播方向与转子转动方向相同

其相对静止坐标系的量纲一转速随转子转速的增大而减小

对这一规律产生的原因进行了分析.

Abstract

An experiment with static and dynamic acquisition were carried out on a transonic compressor rotor at three rotating speed.The analysis was performed on the original signal

the FFT(fast Fourier transform)and the wavelet method.The results show that the stall inception is spike type of whole span.Only one stall cell exists in the flow field

the spreading direction of which is the same as the rotor rotating.And the relative rotating speed of the stall cell decreases when the rotor speed increases.

关键词

Keywords

references

Views

657

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Identification of flexible nozzle torque properties based on wavelet neural network optimized by genetic algorithm

Research for online detection of aerodynamic instability while aero⁃engine test

Aerodynamic characteristics and lift enhancement mechanism of mini-TED in transonic flow

Analysis on tip flow structure in transonic fan rotor

Effect of bulk swirl on performance and stability of transonic single rotor

Related Author

Hongcheng YANG

Shan LIU

Guangzai JIN

Weiwei JIAO

Yufeng JIANG

Zhiyou LIU

Zhilin ZHANG

Ming ZHONG

Related Institution

Laboratory of Aerospace Servo Actuation and Transmission，Beijing Institute of Precision Mechatronics and Controls

Science and Technology on Altitude Simulation Laboratory， Sichuan Gas Turbine Establishment， Aero Engine Corporation of China

College of Energy and Power Engineering，Nanjing University of Aeronautics and Astronautics

National Key Laboratory of Science and Technology on Rotorcraft Aeromechanics, College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics

School of Power and Energy,Northwestern Polytechnical University

AI问答

Postal code：100079
Tel：（010）53879206 Email：tmw@bjxintong.com.cn
Technical support is provided by Beijing Founder electronics co., LTD 京ICP备09082226号-64 京公网安备11010602201714号
It is recommended to read the content of this site in Chrome&IE9+. Please switch to extreme mode in browser 360.
Cookies We use cookies to help provide and enhance our service and tailor content. By continuing, you agree to the use of cookies.

⁰