Thermodynamics First Law of Thermodynamics Steady Flow Energy Equation

A re-entry module flies with Mach 10 at an ambient temperature of -27°C with C_P = 840 J/kg-K, gas constant R = 140 J/kg-K. What is the stagnation temperature at the tip of the nose of the re-entry module?

1

-23°C

2

1377°C

3

2433°C

4

-253°C

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