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)
Relative efficiencies of large landplanes and flying boats
Aeroplane
Aeroplane ; 76 , n 1893
1949
Aufsatz (Zeitschrift)
Englisch
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Relative efficiencies of large landplanes and flying boats
Engineering Index Backfile | 1949
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