Rear wing analysis

I am trying to simulate airflowover my rear wing to get values od drag and lift on the airfoil. However, when I run my simulation my velocity is coming as a single contour in the entire region. Also can you, on a side note, explain how I am supposed to create a body of influence if I can only have one fluid domain.

Here is my project - SimScale Login

Hi @jahnavigupta, thanks for posting on the forum :slight_smile:

Welcome to the SimScale Community :handshake:

Your contour plots look fine to me, is the iterations number (1) set to 1000 on your end?

In order to see more variation, what you can also do is to change the range and limits on the legend bar (2), as per in this Knowledge Base article:

Best,
Igor