Curves show relation between ratio of exhaust pressure to inlet manifold pressure, inlet manifold pressure, and inlet mixture temperature at incipient knock.


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    Title :

    Effect of exhaust pressure on knock-limited performance of air-cooled aircraft-engine cylinder


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1948


    Size :

    22 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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