Hello All,
I am carrying out a flow simulation on an airfoil and am working on post-processing the results. I am trying to compute the skin friction coefficient () on the airfoil surface to identify flow separation and reattachment points. To do this, I need to compute the local wall shear stress ().
Could you please provide guidance on the best way to compute wall shear stress at each point on the airfoil surface?
Any alternative/quick method is appreciated too.
Thank you,
Bharathwaj