6.18 Consider frictionless, incompressible flow of air over the wing of an airplane flying at 200 km

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6.18 Consider frictionless, incompressible flow of air over the wing of an airplane flying at 200 km hr. The air approaching the wing is at 65 kPa and −10 C. At a certain point in the flow, the pressure is 60 kPa. Calculate the speed of the air relative to the wing at this point and the absolute air speed.

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