Question: A wing generates a lift (mathscr{L}) when moving through sea-level air with a velocity (U). How fast must the wing move through the air at
A wing generates a lift \(\mathscr{L}\) when moving through sea-level air with a velocity \(U\). How fast must the wing move through the air at an altitude of \(10,000 \mathrm{~m}\) with the same lift coefficient if it is to generate the same lift?
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