Response of hypothetical aircraft engine cylinder to changes in supercharger compression ratio (boost) and cylinder compression ratio is developed theoretically and outlined by means of charts; attempt made to discuss possibilities of high octane fuels from standpoint of engine designer.


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    Titel :

    High output in aircraft engines, R


    Weitere Titelangaben:

    Soc Automotive Engrs -- J


    Beteiligte:
    DuBois, R.N. (Autor:in) / Cronstedt, V. (Autor:in)


    Erscheinungsdatum :

    1937


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    High-output aircraft engines

    Hives, E.W. / Smith, F.L. | Engineering Index Backfile | 1940


    High-Output Aircraft Engines

    Hives, E. W. / Smith, F. Ll. | SAE Technical Papers | 1940


    High Output in Aircraft Engines

    Bois, Du / Cronstedt, Val | SAE Technical Papers | 1937


    Altitude performance of high-output aircraft engines

    DuBois, R.N. | Engineering Index Backfile | 1941


    ALTITUDE PERFORMANCE of High-Output Aircraft Engines

    DuBOIS, R. N. | SAE Technical Papers | 1941