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