The compressor pressure ratio is 120 and the turbine inlet, Physics

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The compressor pressure ratio is 120 and the turbine inlet

In Professor John L. Krohn's laboratory at Arkansas Tech University, air enters the compressor of an ideal Brayton cycle at p₁= 14.5 psi, T₁= 70.0°F with a volumetric flow rate of 20.0 × 10³ ft³ /min. The compressor pressure ratio is 12.0 and the turbine inlet temperature is 2500.°F. Using the hot air standard cycle analysis, determine the:

a. Net work output of the cycle in Btu/hr and MW.

b. Hot ASC thermal efficiency of the cycle.

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Physics: The compressor pressure ratio is 120 and the turbine inlet

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