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. (Translation) (See also Schweizerische Bauzeitung vol. 95, no. 14, Apr. 5, 1930 pp. 181-186, 16 figs.)
Design of tapered monoplane wings
Zur Berechnung von spitzendigen Eindecker-Trafluegeln
1930
20 pages
16 Figs.
Article (Journal)
English
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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