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Influence Mechanism of Non-Axisymmetric Endwall on Flow Field of Turbine Cascade under Shock Wave Interference

CAO Zhiyuan SONG Zhigao HAO Xinyu WANG Liangfeng YANG Na

热科学学报（英文版）2026，Vol.35Issue(1)：82-96,15.

热科学学报（英文版）2026，Vol.35Issue(1)：82-96,15.DOI:10.1007/s11630-025-2193-3

Influence Mechanism of Non-Axisymmetric Endwall on Flow Field of Turbine Cascade under Shock Wave Interference

CAO Zhiyuan ¹SONG Zhigao ²HAO Xinyu ¹WANG Liangfeng ¹YANG Na³

作者信息

1. School of Power and Energy,Northwestern Polytechnical University,Xi'an 710072,China
2. National Key Laboratory of Science and Technology on Aerodynamic Design and Research,Northwestern Polytechnical University,Xi'an 710072,China
3. High Speed Aerodynamic Institute,China Aerodynamics Research and Development Center,Mianyang 621000,China
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摘要

关键词

non-axisymmetric endwall/transonic turbine cascade/shock wave/secondary flow/passage vortex

Key words

non-axisymmetric endwall/transonic turbine cascade/shock wave/secondary flow/passage vortex

引用本文复制引用

CAO Zhiyuan,SONG Zhigao,HAO Xinyu,WANG Liangfeng,YANG Na..Influence Mechanism of Non-Axisymmetric Endwall on Flow Field of Turbine Cascade under Shock Wave Interference[J].热科学学报（英文版）,2026,35(1):82-96,15.

基金项目

This work is sponsored by the foundation of National Key Laboratory of Science and Technology on Aerodynamic Design and Research. （）

热科学学报（英文版）

ISSN：1003-2169

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