The research progress on partial turbomachinery technology of high-bypass-ratio turbofan engine were reviewed and analyzed in the present study and the partial key technology of turbomachinery required for our country's high-bypass-ratio turbofan engine were also expatiated.The main contents included four aspects: fan/compressor design technique
turbine design technique
flow and noise control and multi-disciplinary coupling technique.
Test of high-bypass-ratio turbofan engine jet noise reduction
Comparison of computation models for simulation of turbomachinery rotor-stator interactions
A viscous inverse problem method for turbomachinery three-dimensional blade profile
New approach to improve the endwall flow of compressor—leading edge strake blade technique
Applicability of blended blade and endwall under different operating conditions
Related Author
ZHOU Xunhuang
GAO Kang
LIU Changchun
宁方飞
杜鹏程
JU Peng-fei
JIA Xin-liang
NING Fang-fei
Related Institution
北京航空航天大学 能源与动力工程学院
北京航空航天大学 航空科学与工程学院
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamic, School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics