Design study; both types designed to fly at 250 mph at 20,000 ft carrying payload of 22,000 lb; powered by four engines of 3000 bhp; considerations of economics and safety. Before joint meeting of Inst Aeronautical Sciences and Roy Aeronautical Soc. (see also Flight v 55 n 2112 June 10 1949 p 716-7)


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    Title :

    Relative efficiencies of large landplanes and flying boats


    Additional title:

    Aeroplane


    Contributors:

    Published in:

    Aeroplane ; 76 , n 1893


    Publication date :

    1949


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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