Research Article
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 = | System 3 Exit | Possible mixture of super-heated steam and saturated vapor. | P = 7 kPa. |
|
|