If an airplane travels at a speed of (1120 mathrm{~km} / mathrm{hr}) at an altitude of (15

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If an airplane travels at a speed of \(1120 \mathrm{~km} / \mathrm{hr}\) at an altitude of \(15 \mathrm{~km}\), what is the required speed at an altitude of \(8 \mathrm{~km}\) to satisfy Mach number similarity? Assume the air properties correspond to those for the U.S. standard atmosphere.

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Ali Khawaja

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