Question
I know the correct answers for are:
a) 34.36MW
b) 0.741
c) 52.2 MW, 870.3 kj/kg
i am just unsure of the methods.
Question 2 Air enters the compressor of a jet engine at 235 K and 40 kPa, with a flow rate of 60 kg/s and speed of 250 m/s. T
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Answer #1

que a consider a one compressor with given condition 7 Q = 1.56 mw comp TI =235% P = 40 kpa m = 60K915 VI = 250 MIS to To = 80 1005 (935-804) +(250 - 2000 60 - 32.7987x18² 1.584183 = w w = -34.358x103 kW I w=-34.358 mW - Negative sigo mdicates that w77 isentropic officienly nisem - Wison Wactural = T2-T Tal-J1 we already know Tal but ... PRIH T Now Find out T2 PI 0.4 R = 2

for speacific heat transfer rate there I taken value of MW so final ans is 568.83Mw/kg.

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I know the correct answers for are: a) 34.36MW b) 0.741 c) 52.2 MW, 870.3 kj/kg...
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