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)


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    Title :

    Liquid-cooled aero engines


    Additional title:

    Aeroplane


    Contributors:
    Wood, H. (author)

    Published in:

    Aeroplane ; 51 , n 1313


    Publication date :

    1936


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Liquid-cooled aero engines

    Wood, H. | Engineering Index Backfile | 1936


    Liquid-Cooled Aero Engines

    Wood, H. | SAE Technical Papers | 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