Hi all I am writing or trying to write something exiciting using deal.ii and as a test of what I have done I wish to solve an airfoil case for a NACA 2408 chord length 1m in 2D. I want to know in general how the solution should flow for example import geometry > mesh geometry > create Dofs etc etc.....
To give a bit of context I have written substantial bindings to the deal.ii repo in python over and above what deal.ii has covered itself in python. I want to test my bindings. However the solutions I am implementing right now are akin to blow ups. compressible flow, rho blows up and incompresible flow I dont get sensible p, u solvers. I think I am missing a solution step which is why the problem might be ill conditioned. Some help might go a long way here. Best Gaurang -- The deal.II project is located at http://www.dealii.org/ For mailing list/forum options, see https://groups.google.com/d/forum/dealii?hl=en --- You received this message because you are subscribed to the Google Groups "deal.II User Group" group. To unsubscribe from this group and stop receiving emails from it, send an email to [email protected]. To view this discussion visit https://groups.google.com/d/msgid/dealii/241634a5-7643-490d-b281-8d1fc56d776fn%40googlegroups.com.
