High Accurate Finite Volume Method for Large Eddy Simulation of Complex Turbulent Flows

Lan Xu,; Guixiang Cui,; Chunxiao Xu,; Zhishi Wang,; Zhaoshun Zhang,; Naixiang Chen,

doi:10.1515/TJJ.2006.23.3.191

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High Accurate Finite Volume Method for Large Eddy Simulation of Complex Turbulent Flows

Lan Xu, , Guixiang Cui, , Chunxiao Xu, , Zhishi Wang, , Zhaoshun Zhang, and Naixiang Chen,

Published/Copyright: September 1, 2006

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From the journal International Journal of Turbo and Jet Engines Volume 23 Issue 3

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Xu,, Lan, Cui,, Guixiang, Xu,, Chunxiao, Wang,, Zhishi, Zhang,, Zhaoshun and Chen,, Naixiang. "High Accurate Finite Volume Method for Large Eddy Simulation of Complex Turbulent Flows" International Journal of Turbo and Jet Engines, vol. 23, no. 3, pp. 191-210. https://doi.org/10.1515/TJJ.2006.23.3.191

Xu,, L., Cui,, G., Xu,, C., Wang,, Z., Zhang,, Z. & Chen,, N. (). High Accurate Finite Volume Method for Large Eddy Simulation of Complex Turbulent Flows. International Journal of Turbo and Jet Engines, 23(3), 191-210. https://doi.org/10.1515/TJJ.2006.23.3.191

Xu,, L., Cui,, G., Xu,, C., Wang,, Z., Zhang,, Z. and Chen,, N. () High Accurate Finite Volume Method for Large Eddy Simulation of Complex Turbulent Flows. International Journal of Turbo and Jet Engines, Vol. 23 (Issue 3), pp. 191-210. https://doi.org/10.1515/TJJ.2006.23.3.191

Xu,, Lan, Cui,, Guixiang, Xu,, Chunxiao, Wang,, Zhishi, Zhang,, Zhaoshun and Chen,, Naixiang. "High Accurate Finite Volume Method for Large Eddy Simulation of Complex Turbulent Flows" International Journal of Turbo and Jet Engines 23, no. 3 (): 191-210. https://doi.org/10.1515/TJJ.2006.23.3.191

Xu, L, Cui, G, Xu, C, Wang, Z, Zhang, Z, Chen, N. High Accurate Finite Volume Method for Large Eddy Simulation of Complex Turbulent Flows. International Journal of Turbo and Jet Engines. ;23(3): 191-210. https://doi.org/10.1515/TJJ.2006.23.3.191

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CONTENTS
Blade Design and Thrust Performance for a Miniature Turbojet Engine
A Numerical Study on Passive Control of Cavity Induced Pressure Oscillations in Two-Dimensional Supersonic Flow
Nonlinear Oscillations in Compressor under Rotating Inlet Distortions
CFD Prediction of Supersonic Ejectors Performance
Probabilistic Analysis of Gas Turbine Field Performance
High Accurate Finite Volume Method for Large Eddy Simulation of Complex Turbulent Flows

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https://doi.org/10.1515/TJJ.2006.23.3.191

Articles in the same Issue

CONTENTS
Blade Design and Thrust Performance for a Miniature Turbojet Engine
A Numerical Study on Passive Control of Cavity Induced Pressure Oscillations in Two-Dimensional Supersonic Flow
Nonlinear Oscillations in Compressor under Rotating Inlet Distortions
CFD Prediction of Supersonic Ejectors Performance
Probabilistic Analysis of Gas Turbine Field Performance
High Accurate Finite Volume Method for Large Eddy Simulation of Complex Turbulent Flows