Calculate the total compressor air mass flow

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An auxiliary gas turbine for use on a large airliner uses a single shaft configuration with air bled from the compressor discharge for aircraft services. The unit must provide 1.5 kg/s bleed air and a shaft power of 200 kW. Calculate (a) the total compressor air mass flow and (b) the power available with no bleed flow, assuming the following:

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Reference no: EM131112996

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