Need help in solving. I'm not getting the correct scalar plots for my case... i.e a car , external aerdynamics.
Thanks in advance.
Im using simple foam.
I can mail system scripts.
Plz help .! :(
We need a bit more information than this.
What are you trying to plot?
What are you using to plot the data?
Is your solution converged?
What is the output of checkMesh?
Solver settings? Boundary conditions? etc.
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