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 translation in Nat. Advisory Committee Aeronautics -- Tech. Memo., no. 649, Dec. 1931, 11 pp., 13 figs. on supp. plates)


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    Title :

    Liquid cooling of aircraft engines


    Additional title:

    Versuche mit Heisskuehlung am Flugmotor


    Contributors:

    Published in:

    Publication date :

    1931


    Size :

    6 pages


    Remarks:

    15 Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    German




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