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2D Mixing Layer Validation Case

K-kL-MEAH2015m Model Results
 

Link to k-kL-MEAH2015m equations

K-kL-MEAH2015m - u velocity at x=200mm K-kL-MEAH2015m - specific turbulent shear stress at x=200mm

K-kL-MEAH2015m - u velocity at x=650mm K-kL-MEAH2015m - specific turbulent shear stress at x=650mm

K-kL-MEAH2015m - u velocity at x=950mm K-kL-MEAH2015m - specific turbulent shear stress at x=950mm

Previously on this page the results were reported as k-kL-MEAH2015 solutions, but more properly they should be referred to as k-kL-MEAH2015m. Essentially no difference is expected.

Note that thorough grid studies were not performed for validation cases such as this one. Some effort was made to ensure reasonable grid resolutions, but there may still be small noticeable discretization errors. Therefore, these validation results shown should be considered representative, but not "truth."

K-kL-MEAH2015m results are shown for CFL3D and FUN3D on the second-finest grid (369x369, 89x161, 121x161). Both CFL3D and FUN3D used freestream turbulence intensity=0.064% and freestream turbulent viscosity (relative to laminar)=0.009 (additional details can be found in the CFL3D User's Manual, Appendix H). Please read note 5 on Notes on running CFD page. Results are nearly identical between the two codes. The y value is normalized by the vorticity thickness (from experiment), the U velocity is normalized by the lower-stream U velocity as well as the change in the U velocity between lower and upper streams. The specific turbulent shear stress is normalized by the square of the change in U velocity. Note that these are compressible code results at "essentially incompressible" conditions of M=0.121108. There may be a very small influence of compressibility. The data files from CFL3D are given here: mixinglayer_cfl3d_u_kkl.dat, mixinglayer_cfl3d_uv_kkl.dat. (Note: some of the profiles have been interpolated using Tecplot software onto pre-set points, that may or may not correspond to the actual grid points or grid cells used in the computation.) A typical FUN3D input file is: fun3d.nml_typical_kkl_2.


 
 

Jump to: SA ResultsSSTm ResultsSST-Vm ResultsSSG/LRR-RSM-w2012 ResultsWilcox2006-klim-m ResultsEASMko2003-S Results

Return to: Mixing Layer Validation Intro Page

Return to: Turbulence Modeling Resource Home Page


 
 


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Last Updated: 02/27/2025