![]() ![]() For a while but once I fly down it gets and stay possitive.Įven if I look at aoa indicators they have mostly only possitive values and books or so show you lift coeficient curve but I have not seen anything which shows how alpha changes in real flight. I can imagine reaching negative alpha during the pushing. My point is that even if I nose dive the flight path vector will be always "under" the airflow. I have airfoil, I put it into a wind tunnel and I can have any aoa I want.īut in reality? Let's asume I have normal real aircraft with some normal angle of incidence. Is it possible to achieve flying at negative angle of attack? Let's skip the part where it would be more like fall than a flight.
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June 2023
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