Distortion of wing under air load causing reduction or reversal of aileron control, weakness in torsion and probability of wing flutter is discussed; increased profile drag; weight; utilization of wing covering for strength; principle of Mono-Spar system; comparison of single and two-spar structures; experimental test wing; wing tip construction. (see also Nat. Advisory Committee for Aeronautics -- Tech. Memorandums, no. 538, Nov. 1929, 14 pp., 8 figs.; and translation in Aerophile, vol. 37, no 17/18, Sept. 1/15, 1929, p. 284, 1 fig)
Cantilever wings for modern aircraft
Aircraft Eng
Aircraft Engineering ; 1 , n 6
1929
4 pages
10 Figs.
Article (Journal)
English
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Cantilever wings for modern aircraft
Engineering Index Backfile | 1929
|Cantilever Wings for Modern Aircraft
Emerald Group Publishing | 1929
|Cantilever wings for modern aircraft
Engineering Index Backfile | 1929
|Engineering Index Backfile | 1929
|Engineering Index Backfile | 1929
|