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. (translation) (See also Aircraft Eng., vol. 1, no. 6, Aug. 1929, pp. 187-190, 10 figs.; Nat. Advisory Committee for Aeronautics -- Tech. Memorandums, no. 538, Nov. 1929, 14 pp., 8 figs.)
Cantilever wings for modern aircraft
Aerophile,
Aerophile ; 37 , n 17/18
1929
1 Fig.
Aufsatz (Zeitschrift)
Englisch
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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
|