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A re-entry module flies with Mach 10 at an ambient temperature of –27°C with. CP = 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?
Here's how I solved the question. Please ignore the (c) at the end of the solution.
Required, but never shown
7 months ago