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Frontiers in Energy >> 2008, Volume 2, Issue 3 doi: 10.1007/s11708-008-0041-2

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

Available online: 2008-09-05

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Abstract

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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