Assume compressible flow-airfoil is moving through the air

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Reference no: EM13709630

An airfoil is moving through the air at 300 mph at 15,000ft pressure altitude. The temperature recorded is 45F.(Assume Compressible Flow)

At a point on the airfoil upper surface is 360 mph. What is the pressure at this point? if this be the average pressure on the surface, how much lift per square foot is being provided by top surface?

Reference no: EM13709630

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