Brief resume of development of Rolls-Royce Kestrel engine and analysis of requirements of high-performance engine of future, developing at least 1500 bhp and operating on fuels of high knock ratings; problems investigated include those of engine forms, fuels, detonation, waste-heat disposal, cooling drag, cooling medium, and mechanical and operational features; conclusions deduced. (See also Soc Automotive Engrs -- J v 39 n 1 and 4 July 1936 p 267-86 (discussion) 286-7 and Oct p 400 and 424)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Liquid-cooled aero engines


    Weitere Titelangaben:

    Aeroplane


    Beteiligte:
    Wood, H. (Autor:in)

    Erschienen in:

    Aeroplane ; 51 , n 1313


    Erscheinungsdatum :

    1936


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Liquid-Cooled Aero Engines

    Wood, H. | SAE Technical Papers | 1936


    Liquid-cooled aero engines

    Wood, H. | Engineering Index Backfile | 1936


    Radial air-cooled aero engines

    Fedden, A.H.R. | Engineering Index Backfile | 1924


    British water-cooled aero engines

    Fell, L.F.R. | Engineering Index Backfile | 1930


    British Water-Cooled Aero Engines

    Fell, Lieut-Col. L.F.R. | Emerald Group Publishing | 1929