What is the net upward force on an airplane wing of area \$20 m^2\$ if the speed of airflow is 300 m/s across the top of the wing and 280 m/s across the bottom? Density of air is \$1.29 kgm^{-3}\$.

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Anonymous · Accepted Answer

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What is the net upward force on an airplane wing of area \\\\(20 m^2\\\\) if the speed of airflow is 300 m/s across the top of the wing and 280 m/s across the bottom? Density of air is \\\\(1.29 kgm^{-3}\\\\).