Research Article
Benefits of Exergy-Based Analysis for Aerospace Engineering Applications—Part I
Table 4
Numerical results for 1 DOF 1st law analysis.
| System 2 (Pipe) | System 2(Pipe) | System 3 (Turbine) | Turbine | Heat transfer | Pressure drop | Heat transfer | Power | % | kW | % | kPa | % | kW | kW |
| 2.50 | 408.98 | 0 | 0 | 0 | 0 | 4434.93 | 1.25 | 204.49 | 0 | 0 | 0 | 0 | 4319.18 | 0.00 | 0.00 | 0 | 0 | 0 | 0 | 4203.44 | −1.25 | −204.49 | 0 | 0 | 0 | 0 | 4097.95 | −2.50 | −408.98 | 0 | 0 | 0 | 0 | 3992.46 |
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