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Evaluate the front stagnation point temperature

Solve the below problem in detail:

Q: Concorde aircraft flies at Ma ≈ 2.3 at 11-km standard altitude. Estimate the temperature in °C at the front stagnation point. At what Mach number would it have a front stagnation point temperature of 450°C?

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Mechanical Engineering: Evaluate the front stagnation point temperature

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Mechanical Engineering: Evaluate the front stagnation point temperature

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