Air streams horizontally past an air plane. The speed over the top surface is 60 m/s and that under the bottom surface is 45 m/s. The density of air being 1.293 kg/m3, calculate the difference in pressure across the wing.

Air streams horizontally past an air plane. The speed over the top sur

1.	Air streams horizontally past an air plane. The speed over the top surface is 60 m/s and that under the bottom surface is 45 m/s. The density of air being 1.293 kg/m3, calculate the difference in pressure across the wing.
Answer» Air streams horizontally past an air plane. The speed over the top surface is $60 m/s$ and that under the bottom surface is $45 m/s$ . The density of air being $1.293 {kg/m}^{3}$ , calculate the difference in pressure across the wing.

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Air streams horizontally past an air plane. The speed over the top surface is 60 m/s and that under the bottom surface is 45 m/s. The density of air being 1.293 kg/m3, calculate the difference in pressure across the wing.

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