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 airfoil includes the case of a split flap deflected for the case of determine the percentage of change of the following when the split flap is used:
A Lift and drag coefficients at angle of attack.
B The maximum lift Coefficient.
C The stall angle of attack.
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