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.


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    Title :

    FUTURE AIRCRAFT ELECTRICAL LOADS


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    Pre-1964 SAE Technical Papers ; 1906



    Publication date :

    1945-01-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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