Response of hypothetical aircraft engine cylinder to changes in supercharger compression ratio (boost) and cylinder compression ratio is developed theoretically and outlined by means of charts; attempt made to discuss possibilities of high octane fuels from standpoint of engine designer.


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    Title :

    High output in aircraft engines, R


    Additional title:

    Soc Automotive Engrs -- J


    Contributors:


    Publication date :

    1937


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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