1945-01-01

FUTURE AIRCRAFT ELECTRICAL LOADS 450044

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.

SAE MOBILUS

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