Account of research work, of which salient features are summarized, as follows: with thick wing sections increase in lift coefficient can be obtained by use of slot equal in magnitude to that with thin wings; similar result in stalled flight can be obtained with both thick and thin sections; if increased control is required at and beyond stall, particularly at very high angles of incidence, controlled slot or "interceptor" should be used, etc.
Slotted wings and the automatic slot
Engineering
Engineering ; 126 , n 3265
1928
3 pages
11 Figs.
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Engineering Index Backfile | 1928
|Engineering Index Backfile | 1921
Practical experiences with slotted wings of automatic type
Engineering Index Backfile | 1930
|Practical experiences with slotted wings of automatic type
Engineering Index Backfile | 1930
|Engineering Index Backfile | 1927
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