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What is the net upward force on an airplane wing of area 15.9 m2 if the speed of flow is 395 m/s across the top of the wing and 272 m/s across the

What is the net upward force on an airplanewing of area 15.9 m2 if the speed of flowis 395 m/s across the top of the wing and272 m/s across the bottom? Assume thatboth the top and bottom of the wing areat the same altitude and the air density is1.29 kg/m3 .Answer in units of N.

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