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rois1995claude
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The NACA 0021 flow pictures show an iso-volume of the Q-criterion
Co-Authored-By: Claude Opus 5.5 <noreply@anthropic.com> Claude-Session: https://claude.ai/code/session_013YFdgQwrRqCQ2ihG446aNe
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‎_vandv/NACA0021_DDES.md‎

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<img src="/vandv_files/NACA0021_DDES/flow_sst_ddes.png" alt="Instantaneous vortical structures, SST-DDES" style="width: 49%; min-width: 0;" />
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<img src="/vandv_files/NACA0021_DDES/flow_sst_eddes.png" alt="Instantaneous vortical structures, SST-EDDES" style="width: 49%; min-width: 0;" />
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</div>
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**Figure 1** - Instantaneous iso-surfaces of the Q-criterion, which show the vortical structures, coloured by the pressure coefficient: SST-DDES (left) and SST-EDDES (right). With SST-DDES, the shear layer from the leading edge stays a smooth sheet before it rolls up. With SST-EDDES, it breaks up into small, three-dimensional eddies close to the airfoil.
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**Figure 1** - Instantaneous vortical structures: iso-volume of the Q-criterion between 10⁻⁵ and 10⁻³, coloured by the pressure coefficient: SST-DDES (left) and SST-EDDES (right). With SST-DDES, the shear layer from the leading edge stays a smooth sheet before it rolls up. With SST-EDDES, it breaks up into small, three-dimensional eddies close to the airfoil.
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## Problem Setup
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