Illustrated description of experimental AW 52G glider; novel control system; large civil and military designs foreshadowed; span 53 ft 10 in.; height 8 ft 4 in.; length 19 ft 4 in.; wheel track 13 ft 9 in.; wing area 443 sq ft; root chord 12 ft 4 in.; weight with crew 6000 lb; wing loading 13.46 lb/sq ft; max speed 250 mph. (see also Aeroplane v 70 n 1824 May 10 1946 p 547-51)
A.W. flying wing
Flight
Flight ; 49 , n 1950
1946
6 pages
Aufsatz (Zeitschrift)
Englisch
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Engineering Index Backfile | 1946
Online Contents | 1995
Engineering Index Backfile | 1941