Numerical simulation of transonic compressor with inlet distortion based on body-force model

被引：0
|
作者：
Qiu, Jiahui [1 ,2 ,3 ,4 ]
Yang, Chen [1 ,2 ,3 ,4 ]
Zhao, Hongliang [5 ]
Zhang, Min [1 ,2 ,3 ,4 ]
Du, Juan [1 ,2 ,3 ,4 ]
Nie, Chaoqun [1 ,2 ,3 ,4 ]
机构：
[1] Advanced Gas Turbine Laboratory, Institute of Engineering Thermo-physics, Chinese Academy of Sciences, Beijing,100190, China
[2] Key Laboratory of Advanced Energy and Power, Chinese Academy of Sciences, Beijing,100190, China
[3] Innovation Academy for Light-Duty Gas Turbine, Chinese Academy of Sciences, Beijing,100190, China
[4] School of Engineering Science, University of Chinese Academy of Sciences, Beijing,100049, China
[5] School of Energy，Power and Mechanical Engineering, North China Electric Power University, Beijing,102206, China
来源：
Hangkong Dongli Xuebao/Journal of Aerospace Power | 2024年 / 39卷 / 08期
关键词：
D O I：
10.13224/j.cnki.jasp.20220526
中图分类号：
学科分类号：
摘要：
Transonic aerodynamics
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