Design and structural features of high-wing externally braced monoplane, powered with three Cirrus III engines; center engine carefully mounted and cowled; R.A.F.-34 wing profile; first machine is of composite construction, with wooden wing spars and ribs, and wooden fuselage construction; cabin seats four passengers; power loading 18.15 lb. per hp.; wing span 57 ft. 6 in.; unusual wing bracing. (See also Flight vol. 21, no. 9, Feb. 28, 1929 pp. 157-161, 8 figs and Aviation, vol. 26, no. 26, June 29, 1929, pp. 2272-2273, 5 figs)


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    Title :

    The Westland IV commercial monoplane


    Additional title:

    Aeroplane


    Published in:

    Aeroplane ; 36 , n 9


    Publication date :

    1929


    Size :

    4 pages


    Remarks:

    9 Figs


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English