Review of development and possibilities of improved designs; data on fuel consumption and weight; air vs. water cooling; supercharging; sleeve-valve performance; exhaust at pressure of 300 lb. per sq. in. can be used in low-pressure cylinder; compression ignition. (see also abstracts in Flight, vol. 22, no. 23, June 6, 1930, pp. 616-620; Aeroplane, vol. 38, no. 23, June 4, 1930, pp. 1075-1076, 1078 and 1080, 4 figs.; Engineer, vol. 149, no. 3882, June 6, 1930, pp. 628-630, and editorial comment on pp. 635-636, and Automobile Engr., vol. 20, no. 269, July 1930, pp. 255-259, 5 figs)


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    Titel :

    The development and progress of the aero engine


    Weitere Titelangaben:

    Roy. Aeronautical Soc. -- Jl


    Beteiligte:
    Ricardo, H.R. (Autor:in)

    Erschienen in:

    Royal Aeronautical Society -- Journal ; 34 , n 240 ; p 1000-1015


    Erscheinungsdatum :

    1930


    Format / Umfang :

    16 pages


    Anmerkungen:

    5 Figs.


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    The development and progress of the aero engine

    Ricardo, H.R. | Engineering Index Backfile | 1930


    The development and progress of the aero engine

    Ricardo, H.R. | Engineering Index Backfile | 1930


    The development and progress of the aero engine

    Ricardo, H.R. | Engineering Index Backfile | 1930


    AERO-ENGINE DEVELOPMENT

    Emerald Group Publishing | 1940


    Aero engine development

    Engineering Index Backfile | 1935