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

Table 3

Description of test cases for 1 Degree of Freedom (DOF) and 5 cases.

Description	Range
System 2: % Heat transfer	−2 to 2.5 (increments of 1.25%)
System 2: % Pressure loss	0 (frictionless)
System 3: % Heat transfer	0 (adiabatic)