Discussion of problem resulting in design formulas in which induced and profile resistance have been fully considered in determination of best diameters, best thrust distribution, etc. (See also - no. 10 May 28 1925 p 209-213)
The most efficient thrust distribution for airplane propellers
Die gunstigste Schubverteilung fur die Luftschraube bei Berucksichtigung des Profilwiderstandes
1925
16 pages
10 Figs.
Article (Journal)
German
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Static thrust of airplane propellers
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