Engineering, 29.05.2021 03:40, Naysa150724

Air exits the compressor and enters the combustor of a gas turbine engine with a flow rate of 84 kg/s at 800 K. Ethane (C2H6) at 298 K enters the combustor to create an overall equivalence ratio of 0.62. Required:
a. Determine the mass flow rate of fuel, in kg/s.
b. Determine the heat release rate, in kW.
c. Determine the mass fraction of oxygen in the products.
d. Determine the adiabatic flame temperature.

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Air exits the compressor and enters the combustor of a gas turbine engine with a flow rate of 84 kg/...