Aerospace Engineering > GATE 2009 > Compressor Performance
An ideal axial compressor is driven by an ideal turbine across which the total temperature ratio is 0.667.
If the total temperature at turbine inlet is T0=1500 K and specific heat of gas cp=1 kJ/kg/K, the
power drawn by the compressor per unit mass flow rate of air is approximately
If the total temperature at turbine inlet is T0=1500 K and specific heat of gas cp=1 kJ/kg/K, the
power drawn by the compressor per unit mass flow rate of air is approximately
Correct : d
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