THE need of intake-charge cooling for the suppression of detonation in highly supercharged engines is indicated by the authors of this paper. The relation of detonation-limited output to intake-charge temperature under numerous engine design and operating conditions is illustrated.Several different methods of reducing the intake-charge temperature are discussed and evaluated, special emphasis being put on the use of intercoolers, aftercoolers, and secondary-liquid injection. It is shown that the choice of any one of these methods depends largely on the type of engine installation and the use of the airplane.


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    Titel :

    The RELATION COOLING of INTAKE-CHARGE to ENGINE PERFORMANCE


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    HERSEY, D. S. (Autor:in) / DROEGEMUELLER, E. A. (Autor:in) / KUHRT, W. A. (Autor:in)

    Kongress:

    Pre-1964 SAE Technical Papers ; 1906



    Erscheinungsdatum :

    01.01.1944




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Relation of intake charge cooling to engine performance

    Droegemueller, E.A. / Hersey, D.S. / Kuhrt, W.A. | Engineering Index Backfile | 1944


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