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

作者：LIU Hongrui;LIU Jun;JI Lucheng;DU Qiang;LIU Guang;WANG Pei

作者单位：School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, ChinaKey Laboratory of Light-Duty Gas-Turbine, Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, ChinaUniversity of Chinese Academy of Sciences, Beijing 100049, ChinaKey Laboratory of Light-Duty Gas-Turbine, Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, ChinaUniversity of Chinese Academy of Sciences, Beijing 100049, ChinaSchool of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China

中文关键词：Intermediate Turbine DuctUnsteady SimulationReynolds NumberFlow Field Analysis

英文关键词：Intermediate Turbine DuctUnsteady SimulationReynolds NumberFlow Field Analysis

刊名：《热科学学报（英文版）》 2018 (3)

相关项目：向心入流转-静系盘腔流动机理及其控制策略研究

页码/页数：294-303,10

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