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 Aeroplane v 76 n 1893 June 10 1949 p 664, 679)
Relative efficiencies of large landplanes and flying boats
Flight
Flight ; 55 , n 2112
1949
2 pages
Article (Journal)
English
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Relative efficiencies of large landplanes and flying boats
Engineering Index Backfile | 1949
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