An explicit N-S solver has been written at the option of one of three turbulence models:Standard K-ε model is an implicit K-ε model coupled with the explicit N-S solver in a novel way which takes account of multiple time scales by adding an extra term to the dissipation equation
and turbulence model based on RNG method which takes account of unbalance effect by adding an extra term to the dissipation equation.The code has been applied to numerical analysis of the flow in the compressor cascade.Three solutions obtained with the three correspondent turbulence models are compared with the experimental results by Flot
R and Papalion
K.It is shown that the results with later two turbulence models become closer to the experimental results.
Analysis of matching characteristic of transonic tandem stator airfoil and its optimization
Intensity analysis of blades in axial compressor with inlet distortion
Numerical simulation of the effect of total pressure inlet distortion on a compressor rotor
Research on turbofan engine HP-compressor rotor-12 blade tip clearance control
Investigation of off design performance of a transonic compressor with circumferential grooves
Related Author
TAO Yuan
YU Xian-jun
LIU Bao-jie
ZHANG Ming-ming
HOU An-ping
HE Xiao-fan
LI Shao-bin
LIANG Chao
Related Institution
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics,School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
National Key Laboratory of Science and Technology on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
School of Aeronautics Science and Engineering, Beijing University of Aeronautics and Astronautics
School of Aerospace, Tsinghua University
School of Power and Energy,Northwestern Polytechnical University