Tests with clearance distribution varied so that for constant compression ratio of 13.5 spherical auxiliary chambers contained 20, 35, 50 and 70% of total clearance volume; results show variations of power, fuel consumption, explosion pressure, rate of pressure rise, ignition lag, heat loss to cooling water, and motoring characteristics.


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    Title :

    Effect of clearance distribution on performance of compression-ignition engine with precombustion chamber


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Notes


    Contributors:


    Publication date :

    1932


    Size :

    13 pages


    Remarks:

    Supp plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English