Well if you see the lift polar it's kind of trailing edge stall that means flow deceleration starts from trailing edge, after reaching maximum lift at alpha_max, if you still increase the angle of attack beyond max_lift there will be still some lift but with decreasing trend. In case of leading edge still the lift results in an abrupt loss of lift. Additionally there are also numerical artifacts in the computations too. Thanks
sir,
why we r getting lift (Cl) even after stalling AOA?
Well if you see the lift polar it's kind of trailing edge stall that means flow deceleration starts from trailing edge, after reaching maximum lift at alpha_max, if you still increase the angle of attack beyond max_lift there will be still some lift but with decreasing trend. In case of leading edge still the lift results in an abrupt loss of lift. Additionally there are also numerical artifacts in the computations too. Thanks
@@Simulation-Engineer thank u so much🤗
How to return back from viewing a single plot to all those 5 plots ??
Hi you can press "a" on the keyboard to get all the plots.