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Why do moderate tapered wings stall first at mid-wing section and high tapered wings stall at tip first? The effective AoA should be always higher close to the root? (considering no geometric or aerodynamic washout)

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  • $\begingroup$ Please take a look at this answer here and see if it clears your question: aviation.stackexchange.com/a/75333/41375. With taper, the local Cl is actually lower at the root at higher AOA. $\endgroup$ – JZYL Jan 10 at 16:28

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