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Incompressible aerodynamics robustness #99

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In general, the methods are robust for very large Reynolds numbers in terms of the iLES (implicit LES) features of the DG discretizations. We ran the 3D Taylor-Green vortex in the inviscid limit (Re -> inf), so at least in the interior of the domain there is a reasonable behavior. The big question for these cases are boundary layers and there high-orders are no silver bullet, as one still needs to refine quite a lot towards the boundary to resolve the gradients. That in turn leads to high aspect ratios and higher costs in the associated solvers. I think the highest numbers we've been considering are in the range of Re~100k. We did some work with wall modeling in the past, https://onlineli…

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