At 293 deg. fahr. mean temperature of cooling liquid, requisite effective radiator area per horsepower is reduced from original 0.04 to 0.011 sq. m. per hp. (See also Zeit. fuer Flugtechnik und Motorluftschiffahrt, vol. 22, no. 18, Sept. 28, 1931, pp. 541-546, 15 figs.)


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    Title :

    Liquid cooling of aircraft engines


    Additional title:

    Versuche mit Heisskuehlung am Flugmotor


    Contributors:


    Publication date :

    1931


    Size :

    11 pages


    Remarks:

    13 Figs., Supp plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English




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