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NACA 0012 HO discretization schemes
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Hello,
I am trying to run the NACA0012 airfoil case with high order discretization schemes SuperBeeV for velocity divergence. I tried several solver configurations but the simulation always diverges. Does anybody know where is the problem? If SuperBee is not feasible for this case which kind of HO discretization scheme can I use? I already used linearUpwind and everything was ok but I wanted to use HO schemes. I attach the folders of the case. Thank you! |
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