Secondary flow analysis for non-axisymmetric endwall on the high-load compressor cascade
Experimental study of flow friction characteristics for a rotor-stator system with centre inflow of cooling air
Pressure drop characteristics of supercritical aviation kerosene in U-turn tube
ICT assisted detection for remainders in the internal cooling channel of the turbine blade
Related Author
徐宁宁
孔星傲
乐鑫灿
王奉明
WU Ji-chang
LU Xin-gen
ZHU Jun-qiang
LI Fu-qing
Related Institution
中国航空发动机集团有限公司 中国航空发动机研究院
Institute of Engineering Thermophysics, Chinese Academy of Sciences
Graduate University of Chinese Academy of Sciences
National Key Laboratory of Science and Technology on Aero-Engines Aero-thermodynamics, School of Jet Propulsion,Beijing University or Aeronautics and Astronautics
School of Jet Propulsion, Beijing University Aeronautics and Astronautics