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The mass flow rate of air through an aircraft engine is 10 kg/s. The compressor outlet temperature is 400 K and the turbine inlet temperature is 1800 K. The heating value of the fuel is 42 MJ/kg and the specific heat at constant pressure is 1 kJ/kg-K. The mass flow rate of the fuel in kg/s is approximately ___________

🗓 Feb 28, 2023

Answer is "0.3 to 0.35"

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Jennifer 🌐 India
Hello, please post an solution as well
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Muskaan 🌐 India
Nice website
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