Solve with numerical values from the steam table step by step. An ideal Brayton Cycle operates with a pressure ratio of $16.$ Air enters the

cycle at a pressure of $14$ psia and temperature of $80F.$ Air exits the turbine at

a temperature of $860$ F$.$ Assume temperature dependent properties $($Table A$-$

$22E.$

a$.$ Draw the T$-$s diagram

b$.$ Determine the maximum temperature of the cycle

c$.$ Determine the amount of heat added during the cycle

d$.$ Determine the thermal efficiency of the cycle

e$.$ Determine the Carnot efficiency of a Carnot heart engine operating

between the same source and sink temperatures as this cycle

f$.$ If the engine net power output is $2000$ hp $,$ determine the mass flow rate of

the air