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,