How can I calculate the normal force and tangetial force on an airfoil in CFD Post?

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Ijaz Fazil Syed Ahmed Kabir

in that case aerfoil should be aligned with axis, like chord line should be along the axis, then only ur answer will be correct bro

S. PERIYASAMY

Using Lift ,drag and angle of attack calculate the normal and axial force.

Get the lift and drag value in all points in xl sheet and use the relation between lift and normal force along with angle of attack..

Yasser M. Ahmed

In the Ansys post-processor you need first to define a local coordinate system that is aligned with the fluid flow, then use the force function to find the lift and drag forces in this case.