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Experimental and Numerical Investigations of Shock-Wave Boundary Layer Interactions in a Highly Loaded Transonic Compressor Cascade

MENG Fanjie LI Kunhang GUO Penghua GAN Jiuliang LI Jingyin

热科学学报（英文版）2024，Vol.33Issue(1)：158-171,14.

热科学学报（英文版）2024，Vol.33Issue(1)：158-171,14.DOI:10.1007/s11630-023-1929-1

Experimental and Numerical Investigations of Shock-Wave Boundary Layer Interactions in a Highly Loaded Transonic Compressor Cascade

MENG Fanjie ¹LI Kunhang ¹GUO Penghua ¹GAN Jiuliang ²LI Jingyin¹

作者信息

1. School of Energy and Power Engineering,Xi'an Jiaotong University,Xi'an 710049,China
2. Institute of Engineering Thermophysics,Chinese Academy of Sciences,Beijing 100190,China
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摘要

关键词

transonic flow/transonic compressor cascade/shock-wave boundary-layer interaction/shock oscillation

Key words

transonic flow/transonic compressor cascade/shock-wave boundary-layer interaction/shock oscillation

引用本文复制引用

MENG Fanjie,LI Kunhang,GUO Penghua,GAN Jiuliang,LI Jingyin..Experimental and Numerical Investigations of Shock-Wave Boundary Layer Interactions in a Highly Loaded Transonic Compressor Cascade[J].热科学学报（英文版）,2024,33(1):158-171,14.

基金项目

This work has been supported by National Science and Technology Major Project(2017-Ⅱ-0007-0021). （2017-Ⅱ-0007-0021）

热科学学报（英文版）

OAEI

ISSN：1003-2169

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