Question: The data provided for NACA 4 4 1 5 airfoil includes the case of a split flap deflected 6 0 . for the case of

The data provided for NACA 4415 airfoil includes the case of a split flap deflected 60. for the case of Re=6106, determine the percentage of change of the following when the split flap is used:
A. Lift and drag coefficients at 4 angle of attack.
B. The maximum lift Coefficient.
C. The stall angle of attack.
 The data provided for NACA 4415 airfoil includes the case of

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