continues? Why? Is there any difference in the C₁ vs a relation you observed in B1, for airfoil with difference thickness, and different camber? At even higher AOA, what happen to the relationship between C₂ and a? In your own words, describes the flow phenomenon that has occurs. B5: Tabulate and discuss the Stall AOA and maximum C₂ of the 4 airfoil studied. B6: Compute and discuss the lift-curve slopes for the 4 airfoil studied. (15 marks)
Fig: 1