Benefits of Exergy-Based Analysis for Aerospace Engineering Applications—Part I

Table 2

Operating conditions for Systems 1 and 3.

Location	Thermodynamic phase	Thermodynamic state
System 1 Exit	Super-heated steam.	P = 100 kPa, T = 400^∘C
System 3 Exit	Possible mixture of super-heated steam and saturated vapor.	P = 7 kPa.