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Engineering · Mechanical Engineering
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4.16 An airplane is moving through still air at 60 m/s. At some point on the wing, the air pressure is-1200 N/m2 gauge. If the density of air is 0.8 kg/m3, find the velocity of the flow at this point. Carefully list the assumptions you have made in your analysis. Express your answer in terms of the nondimensional pressure coefficient C

Ans:81.2 m/s; C,--0.833

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