Calculate the pressure at this point on the wing

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Reference no: EM13702499

A Boeing 747 is flying at M = 0.7 at an altitude where the temperature is 223.15 K. The density is 0.41268 kg/m3, and the pressure is 26429.7 Pa. The pressure coefficient on a point of the wing is -2. a) Calculate V0. b) Calculate the pressure (in Pa) at this point on the wing if V0 = 241.61 m/s.

Reference no: EM13702499

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