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 - n 1 July 1936 p 267-86 (discussion) 286-7; Aeroplane v 51 n 1313 July 22 1936 p 123-6)


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    Title :

    Liquid-cooled aero engines


    Additional title:

    Soc Automotive Engrs -- J


    Contributors:
    Wood, H. (author)


    Publication date :

    1936


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Liquid-cooled aero engines

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    Wood, H. | SAE Technical Papers | 1936


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