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

Table 5

Numerical results for 1 DOF exergy-based analysis.

System 2 (Pipe)		System 2(Pipe)		System 2 (Pipe)	System 3 (Turbine)		Turbine
Heat transfer		Pressure drop		Exergy destruction	Heat transfer		Power
%	𝑘𝑊	%	𝑘𝑃𝑎	𝑘𝑊	%	𝑘𝑊	𝑘𝑊
2.50	408.98	0	0	−240.14	0	0	4434.93
1.25	204.49	0	0	−120.08	0	0	4319.18
0.00	0.00	0	0	0.00	0	0	4203.44
−1.25	−204.49	0	0	110.31	0	0	4097.95
−2.50	−408.98	0	0	220.64	0	0	3992.46