Air from a jet engine intake is diverted to an ideal-gas air-conditioning system at 100 kPa and

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Air from a jet engine intake is diverted to an ideal-gas air-conditioning system at 100 kPa and 2 208C. as shown in Fig. 10.21. The air leaves the compressor at 600 kPa. The air enters the turbine at 25 8C. Assuming constant specific heats and ideal components. Calculate the low-cycle temperature and the cycle COP. For a cabin cooling load of 3000 kJ/min, calculate the necessary mass flow rate of air.
Air from a jet engine intake is diverted to an
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Thermodynamics for Engineers

ISBN: ?978-1133112860

1st edition

Authors: Kenneth A. Kroos, Merle C. Potter

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