A strong interaction between shock wave and leakage vortex
induced by an intensive inter-impact of rotating motion on abrupt anti-pressure gradient
makes their formations and strengths varied.The vortex breakdown deteriorates the stability and efficiency of compressor and fan.So a model of interaction between shock wave and leakage vortex is formulated.The solution of vortex core movement equations shows that the small initiative vortex core velocity and enhanced initiative vortex core pressure will induce the vortex instability.The high Mach number and circulation gradient outside the vortex core will result in breakdown of the vortex.The analysis of the factors leading to vortex breakdown serves as a foundation for its controlling.
NUMERICAL COMPUTATION OF 3D TURBULENT FLOW IN A TRANSONIC SINGLE ROTOR COMPRESSOR
Numerical application of nonlinear EASM model to the interaction between shock waves /turbulent boundary layer
Comparative study on the numerical computation of convective heat transfer over rough surfaces
Numerical simulation of the effect of blade tip blowing on a low speed axial compressor tip clearance flow
Turbulent combustion flow field calculation for afterburner with heat shied
Related Author
Chen Naixing
Huang Weiguang
Zhou Qian
ZHAO Hui-yong
LEI Bo
LE Jia-ling
YANG Sheng-hua
LIN Gui-ping
Related Institution
Institute of Engineering Thermophysics, Chinese Academy of Sciences
Computational Aerodynamics Institute, China Aerodynamics Research and Development Center
Traction Power State Key Laboratory of Southwest Jiaotong University
School of Aeronautics Science and Engineering, Beijing University of Aeronautics and Astronautics
Key Laboratory of Condition Monitoring and Control for Power Plant Equipment, Ministry of Education,Department of Power,School of Energy and Power Engineering, North China Electric Power University