Hello everybody. I would lik
I would like to know if some of you has got experience in solving steady compressible/transonic aerodynamics with OF, possibly around aeronautical configurations, like airfoils and wings. I think that it would be very helpful for people (like me) who aim at verifying OF and exploring its potential in similar fields of interest to check and compare the case setup in terms of solvers, schemes, solution settings and boundary conditions.
Thanks in advance and have a nice day.
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