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