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Uncertainty Sensors
For visualization of the uncertainties the areas of a shock based on Mach number and pressure gradients, areas of stagnation and surface elements including 1st order critical points of separation and reattachment are marked in the output routines.
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Fig. 21 ONERA M6, very coarse grid — expansion ratio of the grid in the boundary layer |
Additionally the number of marked elements, the points in the boundary layers and the boundary layer thickness were written out as further information.
