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SAE AIR1168/3B
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SAE Aerospace Applied Thermodynamics Manual Aerothermodynamic Systems Engineering and Design (Stabilized: Mar 2025)
standard by SAE International , 03/25/2025
SAE AIR1168/3B – SAE Aerospace Applied Thermodynamics Manual Aerothermodynamic Systems Engineering and Design (Stabilized: Mar 2025)
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. Transfer of heat occurs between these sources and sinks by the combined processes of convection, radiation, and conduction in the following manner:
Product Details
Published:
03/25/2025
File Size:
1 file , 3.7 MB
Note:
This product is restricted and cannot be purchased in the following countries Ukraine, Russia, Belarus