Standard
SAE Aerospace Applied Thermodynamics Manual Aerothermodynamic Systems Engineering and Design
2019-09-24
CURRENT
AIR1168/3A
This section presents methods and examples of computing the steady-state heating and cooling loads of aircraft compartments. In a steady-state process the flows of heat throughout the system are stabilized and thus do not change with time. In an aircraft compartment, several elements compose the steady-state air conditioning load.