For commercial airplanes of between 15,000 and 40,000 lb. in total weight, biplane arrangement developed mainly in Great Britain has on whole an advantage; choice between monoplane and biplane is influenced by stalling speed selected; 20 per cent of paying load of machine lost if present-day commercial biplane were transformed into monoplane; performance, stability and control, wing structure, weight, and torsional strength and rigidity of wing structures are compared. (See also Roy. Aeronautical Soc. -- Jl vol. 33, no. 223, July 1929 pp. 490-517, 10 figs (discussion) p 517-540, 10 figs; Flight, vol. 21, no. 9, Feb. 28, 1929, (Aircraft Eng. Sec.) pp. 162-162h, 5 figs.)
Monoplane or biplane
Aeroplane
Aeroplane ; 36 , n 6
1929
3 Figs.
Aufsatz (Zeitschrift)
Englisch
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Engineering Index Backfile | 1929
|Engineering Index Backfile | 1929
|SAE Technical Papers | 1928
|Biplane and monoplane compared
Engineering Index Backfile | 1932
Biplane and monoplane compared
Engineering Index Backfile | 1932