An aircraft is in flight, and its (mathrm{TAS}=220 mathrm{~m} / mathrm{s}). The ambient temperature is (T=253 mathrm{~K}).

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An aircraft is in flight, and its \(\mathrm{TAS}=220 \mathrm{~m} / \mathrm{s}\). The ambient temperature is \(T=253 \mathrm{~K}\). What is the stagnation temperature on its leading edge?

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