Design and performance data of experimental low-wing monoplane built by Gloucester Aircraft Co.; structure weight is only 26 per cent of total weight; two 40-hp. Salmson 9-cylinder radial engines; full loaded machine weighs 1800 lb. of which 1057 lb. is tare weight; top speed 110 m.p.h.; span 38 ft. (see also Flight, vol. 23, no. 28, July 10, 1931, pp. 667-670, 7 figs; Nat. Advisory Committee Aeronautics -- Aircraft Cir., no. 148, July 1931, 7 pp., 8 figs. on supp. plates)


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    Title :

    First mono-spar monoplane


    Additional title:

    Aeroplane


    Published in:

    Aeroplane ; 41 , n 2


    Publication date :

    1931


    Size :

    5 pages


    Remarks:

    8 Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    First mono-spar monoplane

    Engineering Index Backfile | 1931


    First mono-spar monoplane

    Engineering Index Backfile | 1931


    Single-spar monoplane wings

    Engineering Index Backfile | 1929


    Single-spar monoplane wings

    Engineering Index Backfile | 1929