Numerical simulation of three-dimensional turbulent
flow in multistage axial compressor blade row

doi:10.1007/s11708-008-0041-2

Front. Energy

2008, Vol. 2

Issue (3) : 320-325 https://doi.org/10.1007/s11708-008-0041-2

Numerical simulation of three-dimensional turbulent flow in multistage axial compressor blade row

JIANG Jian¹, LIU Bo², WANG Yangang², NAN Xiangyi²

1.Engine Department of Chinese Flight Test Establishment; 2.National Key Laboratory of Airfoil and Cascade Aero-Dynamics, Northwestern Polytechnical University

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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,

Issue Date: 05 September 2008

Cite this article:

JIANG Jian,LIU Bo,WANG Yangang, et al. Numerical simulation of three-dimensional turbulent flow in multistage axial compressor blade row[J]. Front. Energy, 2008, 2(3): 320-325.

URL:

https://academic.hep.com.cn/fie/EN/10.1007/s11708-008-0041-2
https://academic.hep.com.cn/fie/EN/Y2008/V2/I3/320

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