An analysis is presented of the relationship of various engine factors to knock in preignition in an aircraft engine. From this analysis and from the available experimental data, a method of evaluating the knocking characteristics of the fuel in an aircraft-engine cylinder is suggested.


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    Title :

    The knocking characteristics of fuels in relation to maximum permissible performance of aircraft engines


    Contributors:

    Publication date :

    1939-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English



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