The rotor blade in the first stage of Aachen turbine was added with a fillet structure
and a full three-dimensional viscous numerical simulation was performed to analyze the influence of rotor fillet on the performance of turbine stage and flow fields under the stage environment.The results indicate that the efficiency decreases significantly when the angle between fillet and end wall becomes too small
which should raise more attention in the manufacturing process of rotor blade.The fillet structure decreases the transverse pressure difference near the rotor hub and shroud
and shifts the aerodynamic load to the latter half part of the rotor blade.The fillets at hub and shroud affect the flow field of the rotor mainly at the 0%~55% span and the 70%~100% span
respectively.The upper and lower passage vortexes are close to the midspan of rotor due to the influence of the fillet
leading to increase of the intensity of corner vortex and the loss of second flow near the endwall.
Influence of the root fillet on the flow pattern of an axial turbine rotor
Numerical investigation of effect of radial vane diffuser fillet on performance of centrifugal compressor
Flow field characteristics of a two-dimensional integrated asymmetry-expansion nozzle
Numerical simulation on thrust reverser based on secondary flow for high-bypass-ratio turbofan engine
Investigation of ring aerodynamic throat for solid rocket motor
Related Author
WANG Da-lei
PIAO Ying
CHEN Mei-ning
TANG Hui
NING Fang-fei
XIE Wen-zhong
GUO Rong-wei
LIU Chun-yang
Related Institution
School of Aerospace, Tsinghua University
National Key Laboratory of Science and Technology on Aero-engine Aero-thermodynamics,School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics
School of Power and Energy,Northwestern Polytechnical University
Shenyang Aeroengine Research Institute, Aviation Industry Corporation of China