Numerical simulation of three-dimensional turbulent
flow in multistage axial compressor blade row
1.Engine Department of Chinese Flight Test Establishment; 2.National Key Laboratory of Airfoil and Cascade Aero-Dynamics, Northwestern Polytechnical University
Numerical simulation of three-dimensional turbulent flow in a multistage axial compressor blade row is conducted. A high resolution, third-order ENN scheme is adopted to catch the shockwave and simulate the turbulent flow correctly,
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