Calculate the velocity of the airplane

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Reference no: EM13718266

A pitot static tube on an airplane is flying at standard sea level reads 1.04x10^5 M/m^2.

a) Calculate the velocity of the airplane.

b) If the flow velocity is 100m/s at a given point on the surface of the wing of the airplane, calculate the pressure coefficient, static pressure, and total pressure at this point?

Reference no: EM13718266

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