Necessity for developing means of reducing control forces; principle of operation of spring boost tab; flutter; weight of spring tab; application to recent designs; flight test results; effect of spring boost tab on longitudinal stability; rules which should be followed in using spring tabs. (see also Flight v 48 n 1921 Oct 18 1945 p 424-6)
Control surface spring tabs
Aeronautical Eng Rev
Aeronautical Engineering Review ; 4 , n 12
1945
3 pages
Article (Journal)
English
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Engineering Index Backfile | 1945
|Engineering Index Backfile | 1948
|Emerald Group Publishing | 1947
|Emerald Group Publishing | 1947
|Emerald Group Publishing | 1947
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