Lift Coefficient Calculation Using a Geometric/Solution Adaptive Navier Stokes Solver on Two-Dimensional Cartesian Grids for Compressible and Turbulent Flows

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2017-06-15

Author

Kara, Emre
KUTLAR, AHMET İHSAN
Aksel, Mehmet Haluk

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In this study, two-dimensional geometric and solution adaptive refinement/coarsening scheme codes are generated by the use of Cartesian grid generation techniques. In the solution of compressible, turbulent flows one-equation Spalart-Allmaras turbulence model is implemented. The performance of the flow solver is tested on the case of high Reynolds number, steady flow around NACA 0012 airfoil. The lift coefficient solution for the airfoil at a real-life-flight Reynolds number is compared with the experimental study in literature.

Subject Keywords

Turbulence theory and modelling, Educational assessment, Turbulent flows, Aerodynamics, Navier Stokes equations

URI

https://hdl.handle.net/11511/57762

DOI

https://doi.org/10.1063/1.5004352

Conference Name

36th Meeting of Departments of Fluid Mechanics and Thermodynamics

Collections

Department of Mechanical Engineering, Conference / Seminar

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Citation Formats

E. Kara, A. İ. KUTLAR, and M. H. Aksel, “Lift Coefficient Calculation Using a Geometric/Solution Adaptive Navier Stokes Solver on Two-Dimensional Cartesian Grids for Compressible and Turbulent Flows,” Univ W Bohemia, Fac Mech Engn, Dept Power Syst Engn, Pilsen, CZECH REPUBLIC, 2017, vol. 1889, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/57762.