At match point the compressor and turbine are balanced for
(a) Rotor speed (b) power (c) flow rate (d) all of the above
In simplified matching technique
(a) Bearing losses are neglected (b) compressor efficiency is neglected
(c) Turbine efficiency is neglected (d) varying mass flow consideration is considered
The performance map of a compressor is a funtion of
(a) Mass flow rate and pressure ratio (b) pressure ratio and temperature ratio
(c) Pressure ratio and specific heat ratio (d) pressure ratio and work ratio
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