Aeroplane Construction a Handbook On the Various Methods And Details of Constru

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Aeroplane Construction a Handbook On the Various Methods And Details of Constru
Sydney Camm
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The necessity for increased size, with its inevitable sequence, increased weight, must be realized without a very great addi- tion to the landing speed, the figure for the latter standing at approximately 45-50 m. P. H. This factor greatly influences the maximum wing loading possible, without detrimentally affecting this, so that in the design of the large machine a considerable increase in wing area is unavoidable. This fact practically rules out the monoplane system for the large aeroplane, a
...s, although this arrangement possesses a superior ratio of lift to drag to that of the biplane or multiplane, the great span necessary to obtain the wing area is impracticable. It is quite obvious that to brace adequately a monoplane structure of 100 ft. Span or so, a very complex system would be required, in addition to which the spars would essentially 66 AEROPLANE CONSTRUCTION be of larger and heavier section. The biplane arrangement can be used successfully for spans up to 100 ft. , and, assuming that the future commercial machine will necessitate still greater wing area, it is a feasible supposition that the triplane, or even quadruplane systems will be used.

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