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The following data apply to the auxiliary power unit (APU) on the Boeing 777 (single-shaft unit, driving separate load compressor and generator):
Load Compressor
Mass Flow 3.5 kg/s
Pressure Ratio 3.65
Isentropic efficiency 0.88
Gas turbine
Pressure ratio 12.0
Compressor isentropic efficiency 0.84
Turbine inlet temperature 1390 K
(Combustion deltaP)/(compressor delivery pressure) 0.05
Turbine exhaust pressure 1.04 bar
When operating at 35?C and 1.01 bars at take-off conditions, the unit must supply 200 kW electrical loads.Calculate the airflow required for the gas turbine and the SFC?
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