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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    Titel :

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


    Beteiligte:

    Erscheinungsdatum :

    01.01.1939


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch



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