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3. The pressure at a point on the wing of an airplane is 7.58 X 10 N/m. The airplane is flying with a velocity

 

3. The pressure at a point on the wing of an airplane is 7.58 X 10 N/m. The airplane is flying with a velocity of 70 m/s at free stream density-1.23 kg/m, pressure =8.28x10 N/m. Calculate the pressure coefficient at this point of the wing.

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