In: Mechanical Engineering
a simple ideal Brayton cycle with air as the working fluid has a pressure ratio of 10. The air enters the compressor at 520 R and the turbine at 2000 R. Accounting for the variation of specific heats with temperature, determine (a) the ait temperature at the compressor exit, (b) the back work ratio, and (c) the thermal efficiency.
Pressure ratio rp = 10
Compressor inlet temperature T1= 520R
Turbine inlet temperature to T3 = 2000 R

Since we are considering variable specific heats the specific heat at constant pressure and specific heat at constant volume will be different at different temperatures.
At T1= 520R from ideal gas properties of air tables


At T3 = 2000 R from ideal gas properties of air tables


Process 1-2 is isentropic compression




At Pr2 = 12.47 from ideal gas properties of air




(b)
Process 3-4 is isentropic expansion
We know that





At Pr4 = 17.4 from ideal gas properties of air




The work required by compressor is expressed as



The work done by turbine is expressed as



The back work ratio



(c) The thermal efficiency

Heat supplied



Net work is expressed as



Therefore the thermal efficiency



