A Method for Calculating Axial Turbomachine End Wall Turbulent Boundary Layers

Kang Shun,; Liu Fengjun,; Wang Zhongqi,

doi:10.1515/TJJ.1992.9.2.147

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A Method for Calculating Axial Turbomachine End Wall Turbulent Boundary Layers

Kang Shun, , Liu Fengjun, and Wang Zhongqi,

Published/Copyright: June 1, 1992

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From the journal International Journal of Turbo and Jet Engines Volume 9 Issue 2

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Shun,, Kang, Fengjun,, Liu and Zhongqi,, Wang. "A Method for Calculating Axial Turbomachine End Wall Turbulent Boundary Layers" International Journal of Turbo and Jet Engines, vol. 9, no. 2, pp. 147-156. https://doi.org/10.1515/TJJ.1992.9.2.147

Shun,, K., Fengjun,, L. & Zhongqi,, W. (). A Method for Calculating Axial Turbomachine End Wall Turbulent Boundary Layers. International Journal of Turbo and Jet Engines, 9(2), 147-156. https://doi.org/10.1515/TJJ.1992.9.2.147

Shun,, K., Fengjun,, L. and Zhongqi,, W. () A Method for Calculating Axial Turbomachine End Wall Turbulent Boundary Layers. International Journal of Turbo and Jet Engines, Vol. 9 (Issue 2), pp. 147-156. https://doi.org/10.1515/TJJ.1992.9.2.147

Shun,, Kang, Fengjun,, Liu and Zhongqi,, Wang. "A Method for Calculating Axial Turbomachine End Wall Turbulent Boundary Layers" International Journal of Turbo and Jet Engines 9, no. 2 (): 147-156. https://doi.org/10.1515/TJJ.1992.9.2.147

Shun, K, Fengjun, L, Zhongqi, W. A Method for Calculating Axial Turbomachine End Wall Turbulent Boundary Layers. International Journal of Turbo and Jet Engines. ;9(2): 147-156. https://doi.org/10.1515/TJJ.1992.9.2.147

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Published Online: 1992-06

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CONTENTS
The Effect of the Reynolds Number on the Three-Dimensional Flow in a Straight Compressor Cascade
Direct Numerical Simulation of the Phase Change and Heat Transfer of a Vaporizing Droplet
Loading Effects on the Aerodynamics of an Annular Cascade of Three Dimensional Airf
Shock Wave/Free Shear Layer Interaction
Effects of Pressure Mismatch on Slot Injection in Supersonic Flow
A Method for Calculating Axial Turbomachine End Wall Turbulent Boundary Layers
Calculation of the Flow Along the SI Stream Surface with Inviscid-Viscous Interaction Method

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https://doi.org/10.1515/TJJ.1992.9.2.147

Articles in the same Issue

CONTENTS
The Effect of the Reynolds Number on the Three-Dimensional Flow in a Straight Compressor Cascade
Direct Numerical Simulation of the Phase Change and Heat Transfer of a Vaporizing Droplet
Loading Effects on the Aerodynamics of an Annular Cascade of Three Dimensional Airf
Shock Wave/Free Shear Layer Interaction
Effects of Pressure Mismatch on Slot Injection in Supersonic Flow
A Method for Calculating Axial Turbomachine End Wall Turbulent Boundary Layers
Calculation of the Flow Along the SI Stream Surface with Inviscid-Viscous Interaction Method