For the same engine in Prob. 9.18, fuel is injected and burned in the combustor. The gas temperature at the exit of the combustor is 2ll0°R. Assuming that the heat released per pound of fuel is 1.4 x 107 ., calculate the fuel consumption in /sec. Prob. 9.18 The pressure ratio across the compressor of a given turbojet engine is 11.7. The temperature of the air entering the compressor is T2 = 585°R. The mass flow through the compressor is 200 /sec. Assume that the flow velocities entering and leaving the compressor are equal, that is, V2 = V3. Calculate the power (in horsepower) provided by the compressor. where w. is the compressor work per unit mass of gas.
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