An actual detailed aircraft electrical load analysis is a chore for an ‘IBM’ machine, and is indicative only of a specific airplane under controlled conditions.This paper concerns itself with the problem qualitatively, and attempts to show the trend and the advantages of a single Auxiliary Power System for Aircraft, that single system being the electrical system, and into what magnitude of electrical loads such thinking may lead us.
FUTURE AIRCRAFT ELECTRICAL LOADS
Sae Technical Papers
Pre-1964 SAE Technical Papers ; 1906
1945-01-01
Conference paper
English
Design loads for future aircraft
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