[air_engineer_arsenal]

Hi All
I am new on this community and came here to get some help regarding the blocking for a Swept Wing. Previously I have visiting the community as a guest and got a lot of help regarding wing meshing for a simple rectangular wing in the thread "Structured Hexa Mesh on Wing". I found a nice discussion and different blocking strategies for a rectangular wing which actually helped in understanding new things in ICEM CFD. Now I have a problem in hand regarding the CFD analysis of a simple swept back wing. I need help for blocking the wing. I need to know how the blocking strategy in the above mentioned thread will change when we have a swept back wing or is there a method entirely different for this wing. I am attaching my .tin file in this post. Looking for some good help

Regards