The two-dimensional rotor-stator unsteady flow in an axial compressor is calculated by using Euler equations in absolute frame.The computational grids consist of a rotor grid
a stator grid and a intermediate grid which is designed for the connection of blade rows.The fore-boundary points of this intermediate grid rotate with the rotor blades and the aft-boundary points connect with the stator blades.Since the feature of the moving grid is considered in the Euler equations
so it is unnecesary to use the time-consuming interpolation method for information transmission between rotor and stator blade rows.The results of numerical calculation verify the feasibility of the presented approach for calculation of the rotor-stator unsteady flow.
Numerical study on cross-type multi-stream plate-fin heat exchanger
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Related Author
ZHENG Wen-yuan
SHI Hong
XU Lei
ZHOU Nian-yong
JIANG Yan-long
LI Jun
CAI Guo-biao
TIAN Hui
Related Institution
Aviation Key Laboratory of Science and Technology on Aero Electromechanical System Integration, Nanjing Engineering Institute of Aircraft Systems, Jincheng, Aviation Industry Corporation of China
College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics
School of Astronautics, Beijing University of Aeronautics and Astronautics
Aviation Key Laboratory of Science and Technology on Aero-engine Altitude Simulating, China Gas Turbine Establishment, Aviation Industry Corporation of China, Jiangyou Sichuan
School of Power and Energy,Northwestern Polytechnical University