Requirements of high-temperature cooling liquid; properties of ethylene-glycol; investigation conducted by Materiel Division; dynamometer test of Curtiss V-1570 and D-12 engines; endurance and flight tests of D-12 engine; dynamometer test of high-compression-ratio D-12 engine; extremely low fuel consumption; ratio of installed weight to power of liquid-cooled airplane engine considerably reduced by this system. (Aeronautical Eng. Supp.) (See also Aviation vol. 26, no. 22, June 1, 1929 pp. 2 figs (discussion) p 340-343, 25 figs; Soc. Automotive Engrs. Jl., vol. 25, no. 4, Oct. 1929, pp. 329-340. and West. Flying, vol. 6, no. 4, Oct. 1929, p. 56, 1 fig)


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    Title :

    High temperature liquid cooling


    Additional title:

    Aeroplane


    Contributors:
    Frank, G.W. (author)

    Published in:

    Aeroplane ; 36 , n 26


    Publication date :

    1929


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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