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Transition from Unsteady Flow Inception to Rotating Stall and Surge in a Transonic Compressor

CAO Dongming YUAN Caijia WANG Dingxi HUANG Xiuquan

热科学学报（英文版）2022，Vol.31Issue(1)：120-129,10.

Transition from Unsteady Flow Inception to Rotating Stall and Surge in a Transonic Compressor

CAO Dongming ¹YUAN Caijia ¹WANG Dingxi ¹HUANG Xiuquan¹

作者信息

1. Shaanxi Key Laboratory of Internal Aerodynamics in Aero-Engines,Northwestern Polytechnical University,Xi'an 710072,China
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摘要

关键词

transonic compressor/unsteady flow/precursor/rotating stall/surge

Key words

transonic compressor/unsteady flow/precursor/rotating stall/surge

引用本文复制引用

CAO Dongming,YUAN Caijia,WANG Dingxi,HUANG Xiuquan..Transition from Unsteady Flow Inception to Rotating Stall and Surge in a Transonic Compressor[J].热科学学报（英文版）,2022,31(1):120-129,10.

基金项目

The research was supported by the National Natural Science Foundation of China under Grant No.51976172,National Science and Technology Major Project(2017-Ⅱ-0009-0023),and China's 111 project under Grant No.B17037. （2017-Ⅱ-0009-0023）

热科学学报（英文版）

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ISSN：1003-2169

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