Engineering
Engineering, 28.01.2021 20:00, lizzyhearts

The wall of a rocket nozzle is of thickness L = 25 mm and is made from a high alloy steel for which  = 8000 kg/m3, c = 500 J/kgK and k = 25 W/m. K. During a test firing, the wall is initially at Ti = 25C and its inner surface is exposed to hot combustion gases for which h = 500 W/m2.K and T = 1750C. The outer surface is well insulated.

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