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:
![1046_Transtutors004_b6e367c1-db21-43e9-9528-130ea10f02ab.png](https://secure.tutorsglobe.com/CMSImages/1046_Transtutors004_b6e367c1-db21-43e9-9528-130ea10f02ab.png)