Consider the low-speed flow of air over an airplane wing at standard sea level conditions; the free-stream
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Consider the low-speed flow of air over an airplane wing at standard sea level conditions; the free-stream velocity far ahead of the wing is 100 mi/h. The flow accelerates over the wing, reaching a maximum velocity of 150 mi/h at some point on the wing. What is the percentage pressure change between this point and the free stream?
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Since the airspeeds are relatively low let us for the first and only time in this book assume incompressible flow and use Bernoullis equation for this ...View the full answer
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