SAE Aerospace Applied Thermodynamics Manual Aerothermodynamic Systems Engineering and Design
- Aerospace Standard
Convection between the boundary layer and the outer airplane skin.
Radiation between the external skin and the external environment.
Solar radiation through transparent areas directly on flight personnel and equipment and on the cabin interior surfaces.
Conduction through the cabin walls and structural members.
Convection between the interior cabin surface and the cabin air.
Convection between cabin air and flight personnel or equipment.
Convection and radiation from internal sources of heat such as electrical equipment.
Data Sets - Support Documents
|[Unnamed Dataset 1]|
|Table 3A-1||Load Values at Sea Level and 20,000 Ft|
|Table 3A-2||Values for Temperature and Heat Transfer Coefficient|
|Table 3A-3||Results of Analysis|
|Table 3A-4||Passenger Heat Generation|
|Table 3A-5||Average Values of Heat Transfer Coefficient|
|Table 3A-6||Summation of UA Values|
|Table 3A-7||Heating Load at 20,000 Ft|
|Table 3A-8||Heating and Cooling Loads at Sea Level and 20,000 Ft Altitude|
|Table 3B-1||Performance of Vapor Cycle Systems|
|Table 3B-2||System Summary|
|Table 3B-3||Summary of System COP Values|
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