Design and structural features of high-wing externally braced monoplane, powered with three Cirrus III engines; center engine carefully mounted and cowled; R.A.F.-34 wing profile; first machine is of composite construction, with wooden wing spars and ribs, and wooden fuselage construction; cabin seats four passengers; power loading 18.15 lb. per hp.; wing span 57 ft. 6 in.; unusual wing bracing. (See also Flight vol. 21, no. 9, Feb. 28, 1929 pp. 157-161, 8 figs and Aviation, vol. 26, no. 26, June 29, 1929, pp. 2272-2273, 5 figs)
The Westland IV commercial monoplane
Aeroplane
Aeroplane ; 36 , n 9
1929
4 pages
9 Figs
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
The Westland IV commercial monoplane
Engineering Index Backfile | 1929
The Westland IV commercial monoplane
Engineering Index Backfile | 1929
Emerald Group Publishing | 1929