[yashganatra]

I have followed the Cornell University tutorial.
https://confluence.cornell.edu/displ...Airfoil+-+Mesh

I am able to generate one half of the C-Mesh successfully but not the other half.(i.e. the one which contains the rectangular domain only)
As it's necessary to make the edges biased towards the center of airfoil I used a different biasing type than the one suggested in the tutorial.
I have attached the photo of the mesh generated.

I need some suggestions on the possible solutions or the errors that might have crept in.

Thanks,
Yash