Results of tests carried out at speed of 42 ft per sec in 2-ft wind tunnel in Aeronautical Department of Queen Mary College; maximum chore of airfoils was 2.8 in; percentage of stall at various incidences, for three different wings; burbling disturbance along span of two wings; pigeon wing.
Tapered wing stalling
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 39 , n 296
1935
7 pages
Article (Journal)
English
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Engineering Index Backfile | 1936
|Engineering Index Backfile | 1936
|Engineering Index Backfile | 1935
|Emerald Group Publishing | 1937
On stalling of highly tapered wings
Engineering Index Backfile | 1936
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