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- Wall-pressure power spectral density
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- Spanwise coherence length
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### Unsteady pressure signals (layers of probes at several locations in the computational domain)
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- The first layer is located in the first wall-normal cell and goes all around the airfoil,
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- The second layer is located above the upper side, for longitudinal coordinate greater than 60\% chord and at 25\% of the boundary layer height,
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- The third layer is identical to the latter except it is located at 50\% of the boundary layer height,
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- The fourth layer is located above and parallel to the upper side, for longitudinal coordinate greater than 60\% chord and outside of the boundary layer,
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- The bulb set of probes is located at the location of the recirculation bulb, if it exists, and consists of three layers parallel to the airfoil and just spanning the bulb extent,
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- The wake set of probes is located downstream of the trailing edge to capture the vortex
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shedding frequency.
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## Case $`\mathcal{C}_1`$
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- [Boundary Layer quantities](/../tree/master/DATA/AerodynamicData/wp11)
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