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 Aircraft Eng., vol. 1, no. 6, Aug. 1929, pp. 187-190, 10 figs.; and translation in Aerophile, vol. 37, no 17/18, Sept. 1/15, 1929, p. 284, 1 fig.)
Cantilever wings for modern aircraft
Nat. Advisory Committee Aeronautics -- Tech. Memorandums
1929
14 pages
8 Figs.
Report
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Cantilever wings for modern aircraft
Engineering Index Backfile | 1929
|Cantilever wings for modern aircraft
Engineering Index Backfile | 1929
|Cantilever Wings for Modern Aircraft
Emerald Group Publishing | 1929
|Engineering Index Backfile | 1929
|Engineering Index Backfile | 1929
|