How to plot angle of attack Versus lift coefficient plot?
 

Hello everbody,

Cant we plot the lift coefficient and angle of attack plot at once in fluent? is it that we need to give different velocity components each time for different angle of attack?

I have optimized an airfoil now this gives me a new foil parameters and its difficult ko know the new stall angle, is there any procedure to know it too?

Thanks,
Sanjiv