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A small air turbine with an isentropic efficiency of 80% should produce 270 kJ/kg of work. The inlet temperature is 1000 K and it exhausts to the atmosphere. Find the required inlet pressure and the exhaust temperature. 

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C.V. Turbine actual energy Eq.  

w = hi - he,ac = 270 kJ/kg 

hi = 1046.22 ⇒ he,ac = 776.22 kJ/kg, Te = 757.9 K

C.V. Ideal turbine, Eq. and energy Eq 

ws = w/ηs = 270/0.8 = 337.5 = hi - he,s ⇒ he,s = 708.72 kJ/kg From Te,s = 695.5 K

Entropy Eq.  si = se,s adiabatic and reversible 

To relate the entropy to the pressure use Eq  inverted and standard entropy

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