Compressible flow around 2D profile
Does somebody has solutions of commpressible flow ( non viscous) around general wing profile, in symmetric profile the atack angle can be in 2-3 degrees and small mach number for asymmetric profiles atack angle is 0 for example. if someone has the solution in Euler scheme it would be wonderful, It was told to me that the beam warming Algorithm is fine to this solution.
So if one can jelp me i will be very grateful
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