Task B:
B1:
B2:
B3:
15 marks)
B4:
As small AOA, how do you see C₂ varies with a ?
As AOA increases, does the relationship you observes in B1 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