Question: 1 2 - 2 7 ) An aircraft is designed to cruise at Mach number Ma = 1 . 1 at 1 2 , 0

12-27) An aircraft is designed to cruise at Mach number Ma =1.1 at 12,000 m where the atmospheric temperature is 236.15 K. Determine the stagnation temperature on the leading edge of the wing.

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