An airplane has a mass of 2.0 × 106 kg, and the air flows

Chapter 4, Problem 86GP

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An airplane has a mass of \(2.0 \times 10^6 \mathrm{~kg}\), and the air flows past the lower surface of the wings at \(95 \mathrm{~m} / \mathrm{s}\). If the wings have a surface area of \(1200 \mathrm{~m}^2\), how fast must the air flow over the upper surface of the wing if the plane is to stay in the air? Consider only the Bernoulli effect.

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