I am getting the forces in the panelwise.dat file. Can you tell me how to extract the location of that force acting on the wing/location on the panel? I want to do the FEA for the wing and get the panel-wise forces so that I can apply that in my model of FEA.
I am getting the forces in the panelwise.dat file. Can you tell me how to extract the location of that force acting on the wing/location on the panel? I want to do the FEA for the wing and get the panel-wise forces so that I can apply that in my model of FEA.