A NUMERICAL METHOD FOR PREDICTING TURBINE PROFILE LOSS
涡轮盘腔内流动和传热的数值模拟
Research onstream surface for cooling air mixing and variable thickness flow slice in multi-stage
Effects of loading distribution on a vaned diffuser
Influence of suction-side winglet length on tip leakage flow in compressor cascade
Related Author
Yu Qing
Yang Hong
王美丽
周彬
刘松龄
LUO Lei
LU Shao-peng
WANG Song-tao
Related Institution
th Dept.Beijing University of Aeronautics and Astronautics
th Dept. Harbin Institute of Technology
西北工业大学
School of Energy Science and Engineering, Harbin Institute of Technology
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics,School of Jet Propulsion, Beijing University of Aeronautics and Astronautics