Effects of loading distribution on a vaned diffuser
Steady numerical study of aerodynamic throat formed by round injectors
Secondary flow analysis for non-axisymmetric endwall on the high-load compressor cascade
High enthalpy wind tunnel tests of hypersonic inlets with rectangular section
Related Author
刘火星
周志鸿
周亚鸽
周琨
李慕凡
LIU Bao-jie
CAO Si
XIE Kan
Related Institution
北京航空航天大学航空发动机气动热力国家级重点实验室
中国航空发动机集团中国航空发动机研究院
中国航空工业集团有限公司中国空空导弹研究院
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics,School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
School of Astronautics, Beijing University of Aeronautics and Astronautics