The unsteady 3-D flow fields in a transonic compressor at design point were simulated numerically to study the effect of the bowed and swept rotors on rotor wake fluctuation intensity and transportation progress.The results show that
as compared to the baseline
all three types of bowed or swept rotors weaken the fluctuation intensity of tip leakage vortex and the top fluctuation core of wake at rotor outlet
thus quickening the dissipation during downstream transportation and helping to reduce the unsteady disturbance on the top of stator.The fluctuation intensity of the middle part of swept or bowed rotor wake increases to some extent
and the middle-part low energy fluid of rotor wake intends to move downwards during transportation
so the stator is disturbed stronger at mid-span and near hub.
Study of performance and profile pressure distribution of transonic compressor under rotor-stator interaction condition
Research on transient load for transonic compressor based on dynamic boundaries
Improved viscous inverse design method for three-dimensional turbomachinery blades
Impact of bow shock on tip leakage flow in counter-rotating compressor
Unsteady aerodynamic characteristics of ducted coaxial propeller unmanned aerial vehicle
Related Author
LI Shao-bin
SU Jie-xian
FENG Guo-tai
LI Shaobin
ZHANG Weiya
YANG Caiqiong
GUO Qiannan
李艾挺
Related Institution
Sichuan Gas Turbine Establishment,Aero Engine Corporation of China
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics