机译:Hub aspiration strategies and flow loss analysis of a shock-in type supersonic compressor rotor with negative inlet pre-whirl
Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing, China, School of Aeronautics and Astronautics, University of Chinese Academy of Sciences, Beijing, China, Innovation Academy for Light-duty Gas Turbine, Chinese Academy of Scien;
Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing, China, Innovation Academy for Light-duty Gas Turbine, Chinese Academy of Sciences, Beijing, China;
Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing, China, School of Aeronautics and Astronautics, University of Chinese Academy of Sciences, Beijing, China;
corner separation; hub aspiration; shock-in type rotor; shock wave/boundary layer interaction; counter-rotating compressor;