Dear community,
I am currently trying to simulate an airfoil configuration using Palabos, but I am not able to obtain the grid density matrix to have more refinement in the specific zones close to the flaps and slats. Can someone help me out?
Thanks,
Victor
May you share code and geometry?
Hello,
maybe you can try to inspire yourself by this video: https://www.youtube.com/watch?v=sFMXcg4SKBg
Maybe it helps a bit
Yes! Tell me your email and I’ll send it to you!
Thank you Orestis. I´ve seen the video but the code I need is the grid density function generating the matrix of 0s or 1s that determines the level of refinement on each zone. I already have one but it only creates matrices with all 1, and I do not know how to write a code to only write 1 in the zones closer to the slat cove and flap, and zeros on the other regions.
I’ll to answer to you as soon as possible and with my low level experience with Palabos.