基于节流阀模型跨声速轴流压气机失速特性研究

推进技术 ›› 2013, Vol. 34 ›› Issue (6): 741-746.

基于节流阀模型跨声速轴流压气机失速特性研究

胡江峰¹,竺晓程¹,羌晓青²,赵刚¹,杜朝辉¹

上海交通大学机械与动力工程学院,上海 200240;上海交通大学机械与动力工程学院,上海 200240;上海交通大学航空航天学院,上海 200240;上海交通大学机械与动力工程学院,上海 200240;上海交通大学机械与动力工程学院,上海 200240

发布日期:2021-08-15
作者简介:胡江峰(1981—),男,博士生,研究领域为叶轮机械气动热力学。E-mail:huli2003@163.com

Investigation on Stall Behavior in a Transonic Axial Compressor Based on Throttle Model

School of Mechanical Engineering, Shanghai Jiaotong University, Shanghai 200240, China ;School of Mechanical Engineering, Shanghai Jiaotong University, Shanghai 200240, China ;School of Aeronautics and Astronautics, Shanghai Jiaotong University, Shanghai 200240, China;School of Mechanical Engineering, Shanghai Jiaotong University, Shanghai 200240, China ;School of Mechanical Engineering, Shanghai Jiaotong University, Shanghai 200240, China 

Published:2021-08-15

摘要/Abstract

摘要： 为了研究跨声速轴流压气机失速特性,基于节流阀模型,对跨声速轴流压气机转子NASA Rotor 37进行了数值计算,得到了整个失速过程中的流场分布。结果表明,随着阀门进一步关小,压气机逐渐进入旋转失速,在失速发展过程中,失速团逐渐扩展至10%~20%叶高,并绕着旋转轴以低于转子转速同方向旋转。 

关键词: 失速;压气机;节流阀;失速团 

Abstract: In order to investigate transonic compressor stall inception, the internal flow of transonic axial rotor, NASA Rotor 37was simulated based on throttle model. Thus the flow of stall development was gained and analyzed. The numerical simulations show that, compressor gradually becomes to rotating stall as the throttle closes more. In stall development process, stall cell enlarges to about 10%~20% span gradually, and rotates around the same direction with lower speed than the rotor.

Key words: Stall; Compressor;Throttle;Stall cell

胡江峰,竺晓程,羌晓青,赵刚,杜朝辉. 基于节流阀模型跨声速轴流压气机失速特性研究[J]. 推进技术, 2013, 34(6): 741-746.

HU Jiang-feng¹,ZHU Xiao-cheng¹,QIANG Xiao-qing²,ZHAO Gang¹,DU Zhao-hui¹. Investigation on Stall Behavior in a Transonic Axial Compressor Based on Throttle Model[J]. Journal of Propulsion Technology, 2013, 34(6): 741-746.

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