Details of new light biplane; 103 to 105 m.p.h. top speed; wing span 28 ft. 7 in.; wing section thick; all wings are interchangeable; so is rudder with either of elevators, and vice versa; so is fin with either outer section of tailplane which is designed in three sections; all main bracing wires are of same size and length; Cirrus Mark II engine. (See also Simmonds' "Spartan." Flight vol. 20, no. 1028, Sept. 6, 1928 pp. 765-766, 5 figs; Aeroplane, vol. 35, no. 4, July 25, 1928, p. 230, 1 fig.; also Aviation, vol. 25, no. 9, Aug. 25, 1928, p. 606, 1 fig.)
Simmonds. Simmonds' "Spartan."
Airways
Airways ; 5 , n 1
1928
2 Figs.
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Simmonds. Simmonds' "spartan."
Engineering Index Backfile | 1928
Simmonds. Simmonds' "Spartan."
Engineering Index Backfile | 1928
Simmonds. Simmonds' "Spartan."
Engineering Index Backfile | 1928
Engineering Index Backfile | 1929
Reply by Authors to J.G. Simmonds
AIAA | 1964
|