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.)
Autogiro light plane
Flight
Flight ; 20 , n 35
1928
2 pages
1 Fig.
Aufsatz (Zeitschrift)
Englisch
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Engineering Index Backfile | 1934
Engineering Index Backfile | 1928
|Engineering Index Backfile | 1936
SAE Technical Papers | 1929
|Engineering Index Backfile | 1929
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