Aerospace Engineering > GATE 2024 > Compressible Flow
Consider the following Fanno flow problem: Flow enters a constant area duct at a temperature of 273 K and a Mach number of 0.2 and eventually reaches sonic condition (Mach number = 1) due to friction. Assume γ = 1.4. The static temperature at the location where sonic condition is reached is _______ K (rounded off to 2 decimal places).
Correct : a
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