how to calculate the turbulent input parameters for boundary conditions?
Hi every ones,
I am doing simulation for 3D NACA 0012 wing.
I use 3 different tubulent models:
The boundary conditions are:
My question is how to set the turbulent parameters for the input and output bcs such: k,e,I,L,...
I also want to calculate the lift and drag coefficient acting on the wing surface. But I am not sure about the reference values such: area, length. I set the reference area=chord*span and the reference length=chord. Is this right or wrong?
I want to compare with experimental data from NASA experiment. So, how can I know these turbulent conditions?
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