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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 …

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 …
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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.

asked
User Samuel MacLachlan
by
7.6k points

1 Answer

2 votes

Answer:

answer 8 sorry i just need the points

Step-by-step explanation:

answered
User Marcelog
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8.7k points
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