Link to the Project: SimScale
Description of the project: Doing external aerodynamics simulation of a Supra Mark 5 model. Compare the results between the absence and addition of a CAD-modelled rear wing.
What is going wrong: Pressure doesn’t seem to be visualizing or even solving properly on this wing. I used inspect point and it showed negative pressure all around the wing when it should’ve only been negative on the bottom of the wing.
I had a successful simulation run with a similar model earlier, but this time it doesn’t work, even though I replicated the settings.
Any help would be greatly appreciated!