Hi guys, I’m working on a flow simulation of a front wing for a Formula SAE racecar. I’ve tried following some of the tutorials for other wings, but I’m not completely sure that the numerical parameters I’ve input are correct.

For this simulation, I’m trying to get numbers for a coefficient of drag, coefficient of lift, amount of down force, and center of pressure on the wing. I’m not really sure if I’ve set up the simulation parameters correctly to find these values, but their seems to be a larger problem.

After I ran the simulation and opened it up in the post processor, I wasn’t able to see any values, and the whole mesh box is a single color. This is the first CFD simulation I’ve run, so I honestly have no idea what I’m doing. Any help would be greatly appreciated.

Here’s a link to the project: https://www.simscale.com/projects/wrenda/frontwing_2/

Here’s what the sim currently looks like.