The test results of a NACA 2518 shows: Angle of attack 0 deg 8 deg CL 0.045 0.75 If the airfoil is used to construct a wing with a span of 60 ft and a wing area of 450 square feet. Determine the wing lift curve slope. (e = 0.88)

The test results of a NACA 2518 shows: Angle of attack 0 deg 8 deg CL 0.045 0.75 If the airfoil is used to construct a wing with a span of 60 ft and a wing area of 450 square feet. Determine the wing lift curve slope. (e = 0.88)

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Question

The test results of a NACA 2518 shows:
Angle of attack
0 deg
8 deg
CL
0.045
0.75
If the airfoil is used to construct a wing with a span of 60 ft and a wing area of 450 square feet.
Determine the wing lift curve slope. (e = 0.88)

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