I want to make a simulation for a airfoil for i solute it with FLUENT.
I must use the k-e turbulent model but i do not know how i make the mesh near the wall of airfoil. I have read that the Y plus of first cell must be within 30-300 for standard wall function. However, How can i compute the Y length of cells for i make the mesh arround the foil （NACA0012），and also ,I want some tutorials about ernal flow around airfoil or cylinder with Reynolds number at nearly 50000.
Then calculate friction stress and friction velocity
Then we have
where is the kinematic viscosity
now ,i had done some examples by k-e model ,y+=0.0001m,Angle of Attack is 12(re=50000,the chord length is 1m),but from the result ,i can't find the shedding vortex,may i have your email ? i have some details to talk with you，ok？
looking forward to your reply .merry christmas
May be it is dimension value?
Optimal y+ near the wall is about 1 (dimensionless!) for calculation without wall function and 10-100 for calculation with wall functions. But never 0.0001!
Did you estimate friction velocity u* for your case?
I am not expert in aerodynamics but i think shedding vortex does not obligatory occur. It depends on many circumstances.
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