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mue

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  1. If you could find more information how exactly stall is modelled in SF2, I would be *very* grateful! How the normal flight envelope is modelled I understand quite well: sf2_fdm_notes.pdf. But the stall regime is still rather unknown to me. BTW, the key 'Qr — Downwash/relief factor used in aero build (vs α)' is also unknown to me. And I couldn't find it in any stock aircraft data inis. What exactly is this downwash/relief factor?
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