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)
$\begingroup$
$\endgroup$
1
-
$\begingroup$ 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
Add a comment
|
