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 - (discussion) p 517-540; Flight, vol. 21, no. 9, Feb. 28, 1929, (Aircraft Eng. Sec.) pp. 162-162h, 5 figs., and Aeroplane, vol. 36, no. 6, Feb. 6, 1929, pp. 185-187, 188, 190 and 193, 3 figs)


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    Title :

    Monoplane or biplane


    Additional title:

    Roy. Aeronautical Soc. -- Jl


    Contributors:

    Published in:

    Publication date :

    1929


    Size :

    28 pages


    Remarks:

    10 Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Monoplane or biplane

    Farren, W.S. | Engineering Index Backfile | 1929


    Monoplane or biplane

    Farren, W.S. | Engineering Index Backfile | 1929


    Monoplane or biplane?

    Gymnich, A. | Engineering Index Backfile | 1928


    Monoplane or Biplane

    CHATFIELD, C. H. | SAE Technical Papers | 1928


    Biplane and monoplane compared

    Engineering Index Backfile | 1932