I’m attempting an analysis of an open wheel race car. When I try to calculate the aerodynamic coefficients of the vehicle, I’m left with the result below.
I would like to know the coefficients of the front wing, rear wing, and entire body separately if that’s possible. For each, I created a force coefficient plot through the result control section. I then selected the faces of the each component, entered the planform area of the component and the reference length.