Dear Gmsh Experts,
I'm a newbie with Gmsh and open-source softwares, and as my first
project, I'm trying to do a 2D CFD simulation around an airfoil using
openFOAM. I want to develop a method which I can use in all future CFD
projects. For this reason, I'm trying to simulate flow around a NACA
airfoil, for which standard test data is available. I'm using a c-grid
hexa mesh for the airfoil. Initial trials have produced results which
are a bit erroneous. I believe the problem can be solved by producing a
good boundary layer mesh, with a suitable first layer distance based on
a y+ value. But I cannot find a good source which would guide me through
the process of specifying a first layer distance of the mesh from the
airfoil wall. Kindly tell me a method (set of commands and how to use
them) I can use to do what I intend to do or, if possible, point me to a
source which would give a proper tutorial on how to do a good boundary
layer mesh.
Thanks and regards,
Kushagra Vidyarthi
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