Validating the URANS shear stress transport γ −Reθ model for low‐Reynolds‐number external aerodynamics

DOI10.1002/FLD.2651zbMath1253.76051OpenAlexW1918316430MaRDI QIDQ4898044

J. N. N. Counsil, K. Boulama

Publication date: 29 December 2012

Published in: International Journal for Numerical Methods in Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1002/fld.2651

zbMATH Keywords

transitionURANSNACA0012LSBexternal aerodynamics\texttt{ANSYS-CFX}

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25)

Related Items (1)

Effect of the laminar separation bubble induced transition on the hydrodynamic performance of a hydrofoil

Uses Software

• ANSYS-CFX

Cites Work

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• Direct numerical simulation of flow separation around NACA 0012 airfoil
• Performance of transition model for predicting low \(Re\) aerofoil flows without/with single and simultaneous blowing and suction
• Evaluation of two-equation turbulence models for predicting transitional flows
• Computational Methods for Fluid Dynamics
• Some properties of boundary layer flow during the transition from laminar to turbulent motion
• Numerical study of the turbulent flow past an airfoil with trailing edge separation
• Numerical simulation of thin airfoil stall by using a modified DES approach
• Direct numerical simulations of forced and unforced separation bubbles on an airfoil at incidence
• Industrial application of RANS modelling: capabilities and needs
• Validation of the RANS-simulation of laminar separation bubbles on airfoils
• Dynamics of laminar separation bubbles at low-Reynolds-number aerofoils

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