Comparative study on three Fourier-based time-domain unsteady computation methods
including the shape-correction phase shift method
space-time gradient method and harmonic balance method
was carried out by simulation of two typical kinds of rotor-stator interactions
i.e.:wake-blade interactions and shock-blade interactions. Differences and relations between these computation methods were investigated in detail
and their computational accuracy and speed were also analyzed. The results indicate that three methods can resolve the unsteady flow details well. Compared with the conventional time-marching method
the computational speed of these methods can be enhanced from several to dozens of times
making these methods applicable to daily design process.
Vibration reduction analysis and design of friction ring damper in blisk
Analysis of effect factors on damping characteristics for underplatform dampers
Comparison among three models for compressor internal flow
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
Related Author
QI Wenkai
WEN Wei
陈俊杰
臧朝平
周标
阳刚
陈逖
江雄
Related Institution
南京航空航天大学 能源与动力学院 江苏省航空动力系统重点实验室
中国空气动力研究与发展中心 科技部
中国空气动力研究与发展中心 计算空气动力研究所
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamic, School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics