THIS paper gives a brief resumé of the development of the Rolls-Royce Kestrel engine and then analyzes the requirements of the high-performance engine of the future, developing at least 1500 b.hp. and operating on fuels of high knock ratings.The problems investigated include those of engine form, fuels, detonation, waste-heat disposal, cooling drag, cooling medium, and the mechanical and operational features.Conclusions deduced from the arguments are: THIS paper gives a brief resumé of the development of the Rolls-Royce Kestrel engine and then analyzes the requirements of the high-performance engine of the future, developing at least 1500 b.hp. and operating on fuels of high knock ratings.The problems investigated include those of engine form, fuels, detonation, waste-heat disposal, cooling drag, cooling medium, and the mechanical and operational features.Conclusions deduced from the arguments are: THIS paper gives a brief resumé of the development of the Rolls-Royce Kestrel engine and then analyzes the requirements of the high-performance engine of the future, developing at least 1500 b.hp. and operating on fuels of high knock ratings.The problems investigated include those of engine form, fuels, detonation, waste-heat disposal, cooling drag, cooling medium, and the mechanical and operational features.Conclusions deduced from the arguments are: THIS paper gives a brief resumé of the development of the Rolls-Royce Kestrel engine and then analyzes the requirements of the high-performance engine of the future, developing at least 1500 b.hp. and operating on fuels of high knock ratings.The problems investigated include those of engine form, fuels, detonation, waste-heat disposal, cooling drag, cooling medium, and the mechanical and operational features.Conclusions deduced from the arguments are: THIS paper gives a brief resumé of the development of the Rolls-Royce Kestrel engine and then analyzes the requirements of the high-performance engine of the future, developing at least 1500 b.hp. and operating on fuels of high knock ratings.The problems investigated include those of engine form, fuels, detonation, waste-heat disposal, cooling drag, cooling medium, and the mechanical and operational features.Conclusions deduced from the arguments are:


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    Titel :

    Liquid-Cooled Aero Engines


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Wood, H. (Autor:in)

    Kongress:

    Pre-1964 SAE Technical Papers ; 1906



    Erscheinungsdatum :

    01.01.1936




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Liquid-cooled aero engines

    Wood, H. | Engineering Index Backfile | 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