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cl lcavg C 10 Determine the net work, and the thermal efficiency for the gas turbine shown in the next figure. Knowing that the high pressure turbine is used to drive the compressor. All necessary data are included in the figure and assume that all processes are ideal Exhaust Regenerator Burner Air ntake urbinen150Kw urbine Compressor Turbine P 100 kPa 300 K P-100 kPa -1600 K Please clear hind writing. Cp=1.0004., cv=0.718 . K=1.4
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Given Data K Pa ะ300 K find → Ntt Work aud -thermal E.frceček a に2ラhelt ropic Gwum ewton Tj T2ะ 500 . 55 k Ertno reure drop hEfftci euA of Heat excluau(Jer is 100% 3 2 Ta 3-Ts = 958.9214 K Heat supplied kd :-Oz = CpCtq-13 644.283 KJ / k Heat deppliea

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Please clear hind writing. Cp=1.0004., cv=0.718 . K=1.4 cl lcavg C 10 Determine the net work,...
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