Stating that requirements of airplane power plant are light weight, low fuel, and oil consumption, reliability and durability, smooth and flexible operation and compactness, author discusses briefly how these are obtained; greater proportionate weight of accessories, foundry limitations and other considerations than loads and stresses tend to make small airplane engine heavier in proportion to horsepower than larger power plants, manufacturing costs being more important than maximum performance in power and weight. (See also - discussion p 351 and 371)


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    Titel :

    Small airplane-engines


    Weitere Titelangaben:

    Soc. Automotive Engrs. -- Jl


    Beteiligte:
    Tilley, N.N. (Autor:in)


    Erscheinungsdatum :

    1930


    Format / Umfang :

    6 pages


    Anmerkungen:

    12 Figs.


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Starting of small airplane engines

    Steimle, E. | Engineering Index Backfile | 1938


    Airplane Engines

    Palocz-Andresen, Michael | Springer Verlag | 2012


    Airplane engines

    Engineering Index Backfile | 1930


    Airplane engines

    Engineering Index Backfile | 1932


    Airplane engines

    Capetti, A. | Engineering Index Backfile | 1927