Extract the force and moment component at each grid of the surface marker

[Rashmikant15]

Dear SU2 community,

I have done aerodynamic analysis using SU2, and I want to extract the force (Fx, Fy, Fz) and moment components (Mx, My, Mz) at each grid of the surface marker in a specified order. Ex. from the root chord (leading-edge to trailing-edge) to the tip chord for an aircraft wing.

Thank you so much for the help.

[bigfooted]

I do this in paraview. I have an example for the local and total forces of the unsteady flow over an unsteady cylinder here:
https://github.com/bigfooted/su2cases/tree/master
https://github.com/bigfooted/su2cases/tree/master/validation/unsteady_inc_cylinder_farfield