Analysis of stresses and aerodynamical characteristics of tapered cantilever wings; determination of shape of wing for producing given lift distribution; it is shown that tips of tapered wing are more heavily loaded than middle portion. (see also translation in Nat. Advisory Committee for Aeronautics -- Tech. Mem., no. 578, Aug. 1930, 20 pp., 16 figs.)
Design of tapered monoplane wings
Zur Berechnung von spitzendigen Eindecker-Trafluegeln
Schweizerische Bauzeitung ; 95 , n 14
1930
6 pages
16 Figs.
Aufsatz (Zeitschrift)
Deutsch
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Design of tapered monoplane wings
Engineering Index Backfile | 1930
|Calculation of tapered monoplane wings
NTRS | 1930
|Calculation of tapered monoplane wings
TIBKAT | 1930
|Emerald Group Publishing | 1938
|Engineering Index Backfile | 1929