Prediction of Incompressible Turbulent Separated Flows Using the Viscous Layer Model

J.-Z. Xu,; C.-X. Xiong,; H.-Z. Gao,; B. Chen,

doi:10.1515/TJJ.1996.13.3.183

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Prediction of Incompressible Turbulent Separated Flows Using the Viscous Layer Model

J.-Z. Xu, , C.-X. Xiong, , H.-Z. Gao, and B. Chen,

Published/Copyright: September 1, 1996

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From the journal International Journal of Turbo and Jet Engines Volume 13 Issue 3

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Harvard
Chicago
Vancouver

Xu,, J.-Z., Xiong,, C.-X., Gao,, H.-Z. and Chen,, B.. "Prediction of Incompressible Turbulent Separated Flows Using the Viscous Layer Model" International Journal of Turbo and Jet Engines, vol. 13, no. 3, pp. 183-192. https://doi.org/10.1515/TJJ.1996.13.3.183

Xu,, J., Xiong,, C., Gao,, H. & Chen,, B. (). Prediction of Incompressible Turbulent Separated Flows Using the Viscous Layer Model. International Journal of Turbo and Jet Engines, 13(3), 183-192. https://doi.org/10.1515/TJJ.1996.13.3.183

Xu,, J., Xiong,, C., Gao,, H. and Chen,, B. () Prediction of Incompressible Turbulent Separated Flows Using the Viscous Layer Model. International Journal of Turbo and Jet Engines, Vol. 13 (Issue 3), pp. 183-192. https://doi.org/10.1515/TJJ.1996.13.3.183

Xu,, J.-Z., Xiong,, C.-X., Gao,, H.-Z. and Chen,, B.. "Prediction of Incompressible Turbulent Separated Flows Using the Viscous Layer Model" International Journal of Turbo and Jet Engines 13, no. 3 (): 183-192. https://doi.org/10.1515/TJJ.1996.13.3.183

Xu, J, Xiong, C, Gao, H, Chen, B. Prediction of Incompressible Turbulent Separated Flows Using the Viscous Layer Model. International Journal of Turbo and Jet Engines. ;13(3): 183-192. https://doi.org/10.1515/TJJ.1996.13.3.183

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Published Online: 1996-09

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CONTENTS
Design, Development, and Performance of a Turbine Research Facility to Study Rotor Stator Interaction Effects
Α Study on the Hartmann-Sprenger Tube Flow Driven by a Sonic Jet
Prediction of Incompressible Turbulent Separated Flows Using the Viscous Layer Model
Euler Analysis of Oscillating Cascade Aerodynamics Using Embeded Composite Grids
Technical Note: UV-VIS Absorption as a Diagnostic for NO in Rocket Plumes
Assessment Of Navier-Stokes and Boundary Layeer Procedures for the Prediction of Two-Dimensional Viscous Flow in a Turbine Nozzle

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https://doi.org/10.1515/TJJ.1996.13.3.183

Articles in the same Issue

CONTENTS
Design, Development, and Performance of a Turbine Research Facility to Study Rotor Stator Interaction Effects
Α Study on the Hartmann-Sprenger Tube Flow Driven by a Sonic Jet
Prediction of Incompressible Turbulent Separated Flows Using the Viscous Layer Model
Euler Analysis of Oscillating Cascade Aerodynamics Using Embeded Composite Grids
Technical Note: UV-VIS Absorption as a Diagnostic for NO in Rocket Plumes
Assessment Of Navier-Stokes and Boundary Layeer Procedures for the Prediction of Two-Dimensional Viscous Flow in a Turbine Nozzle