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1 emit 2 ( Marks = 3 0 ) [ Answer in the space provided, show important calculation steps ] A small gas turbine engine
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A small gas turbine engine that drives an air compressor is supplied from a large pipeline with combustion gas at kPa and The turbine exhaust pressure kPa. The gas flow rate is Turbine isentropic efficiency is At the compressor inlet, the pressure and temperature of the air are kPa and respectively. The air flow rate is Compressor isentropic efficiency is
For air compressor: ; For combustion gas:
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