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    Application of Bernoulli's theorem

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    What is the net upward force on an airplane wing of area 17.9 m^2 if the speed of air flow is 295 m/s across the top of the wing and 280 m/s across the bottom.

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    Please refer attachment for solution. However, before looking at the solution try to solve the problem as follows :

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    Solution Summary

    The problem has been solved by applying Bernoulli's theorem.