The unit must provide 15 kgs bleed air and a shaft power of


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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Mechanical Engineering: The unit must provide 15 kgs bleed air and a shaft power of
Reference No:- TGS01490965

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