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Influence of Reynolds Number on the Unsteady Aerodynamics of Integrated Aggressive Intermediate Turbine Duct

LIU Hongrui LIU Jun JI Lucheng DU Qiang LIU Guang WANG Pei

热科学学报（英文版）2018，Vol.27Issue(3)：294-303,10.

Influence of Reynolds Number on the Unsteady Aerodynamics of Integrated Aggressive Intermediate Turbine Duct

LIU Hongrui ¹LIU Jun ²JI Lucheng ³DU Qiang ²LIU Guang ³WANG Pei¹

作者信息

1. School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China
2. Key Laboratory of Light-Duty Gas-Turbine, Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, China
3. University of Chinese Academy of Sciences, Beijing 100049, China
折叠

摘要

关键词

Intermediate Turbine Duct/Unsteady Simulation/Reynolds Number/Flow Field Analysis

Key words

Intermediate Turbine Duct/Unsteady Simulation/Reynolds Number/Flow Field Analysis

引用本文复制引用

LIU Hongrui,LIU Jun,JI Lucheng,DU Qiang,LIU Guang,WANG Pei..Influence of Reynolds Number on the Unsteady Aerodynamics of Integrated Aggressive Intermediate Turbine Duct[J].热科学学报（英文版）,2018,27(3):294-303,10.

基金项目

This work was supported by the National Natural Science Foundation of China (51776200). （51776200）

热科学学报（英文版）

OACSCD

ISSN：1003-2169

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