Details of two-seater Avro Avian airplane fuselage to which has been applied autogiro principle; four blades doubly articulated; monoplane stabilizer wing, semi-cantilever with spruce spars and three-ply and fabric covering at dihedral angle of 5 deg.; A.D.C. Cirrus Mark II, 80-hp. engine; span of stabilizing plane 19 ft. 9 in.; undercarriage track 8 ft. 7 1/2 in.; 90 m.p.h. estimated maximum speed; details of Cierva Autogiro, C.8.L.2 with Armstrong-Siddeley Lynx 180-hp. engine. (See also - no. 27, July 5, 1928, p. 543, 1 fig.)


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    Title :

    Autogiro light plane


    Additional title:

    Flight


    Published in:

    Flight ; 20 , n 35


    Publication date :

    1928


    Size :

    2 pages


    Remarks:

    1 Fig.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Autogiro developments

    Engineering Index Backfile | 1934


    The autogiro

    Bouche´ / H. | Engineering Index Backfile | 1928


    Roadable Autogiro

    Engineering Index Backfile | 1936


    The Autogiro

    DE LA CIERVA, JUAN | SAE Technical Papers | 1929


    The autogiro

    de la Cierva, J. | Engineering Index Backfile | 1929