Products of combustion enter the turbine section of a jet engine at 1200 K with a flow rate of 63.5 kg/s. Determine the turbine outlet temperature if the turbine delivers 28.2 MW to drive the compressor. Assume ideal operation of the turbine and that the properties of the combustion products can be approximated by those of air.

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T₁ = 1200 K T₂=? Combustor Turbine