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 Aeroplane, vol. 41, no. 2, July 8, 1931, pp. 122-126, 8 figs; Nat. Advisory Committee Aeronautics -- Aircraft Cir., no. 148, July 1931, 7 pp., 8 figs. on supp. plates)


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    Titel :

    First mono-spar monoplane


    Weitere Titelangaben:

    Flight


    Erschienen in:

    Flight ; 23 , n 28


    Erscheinungsdatum :

    1931


    Format / Umfang :

    4 pages


    Anmerkungen:

    7 Figs.


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    First mono-spar monoplane

    Engineering Index Backfile | 1931


    First mono-spar monoplane

    Engineering Index Backfile | 1931


    Single-spar monoplane wings

    Engineering Index Backfile | 1929



    Steiger mono-spar

    Engineering Index Backfile | 1932