Major requirements of aircraft engines discussed are: minimum weight per horsepower; minimum consumption of fuel and oil; minimum frontal area or heat resistance; maximum reliability; maximum durability; minimum initial costs; minimum cost of maintenance; speed to secure efficiency and no noise from propeller; maximum unobstructed view ahead for pilot; description of Earl aircraft engine, which is 4-cycle gasoline engine, cylindrical in form, with two-part hollow propeller shaft extending through center of engine; weighs about 1 lb. per hp.


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    Titel :

    A compact aeronautic engine


    Weitere Titelangaben:

    Soc. Automotive Engrs. -- Jl


    Beteiligte:
    Earl, H.W. (Autor:in)


    Erscheinungsdatum :

    1930


    Format / Umfang :

    5 pages


    Anmerkungen:

    4 Figs.


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    A novel aeronautic engine

    Earl, H.W. | Engineering Index Backfile | 1929


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