[patep022]

I am a 3rd year engineering student and my project involves the CFD of a Delta wing. the delta wing geometry is very simple and I was advised to use an unstructured mesh. I am very new to this software and have come across a problem which I cannot seem to figure out.

I attempted to do a volume mesh with the geometry drawn in ICEM. The mesh works as I want it to except on the edges where it is missing out on bits and makes the edge very jaggered.

Please see the attached images to get a better idea of what I am talking about.

I would appreciate any help with this.

Many thanks