Having trouble sleeping so here's a data sci nerd story for you all.
This would be bad in a multi-million dollar tunnel with air moving at 700mph.
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Transonic refers to the range betwern Mach 0.7ish and Mach 1.2ish, depending on structure.
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In transonic flow, air moves at > Mach 1 at some parts of the model, and shockwaves form, but not everywhere
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The transonic range is poorly understood and even our best computational models today perform v poorly.
End of conversation
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Like e.g. what does a dynamics tunnel do that's so complicated?