anom2761
3rd Mar 2010, 12:28
Under what conditions would an aerofoil stall before its actual critical stalling angle?? relating to flow vortex.
Why after an aerofoil has stalled would the Coffeicient of Lift suddenly increase i.e at 20 degrees after the stall?
Why after an aerofoil has stalled would the Coffeicient of Lift suddenly increase i.e at 20 degrees after the stall?