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.
Aufsatz (Zeitschrift)
Deutsch
© Metadata Copyright Elsevier B. V. All rights reserved.
Static thrust of airplane propellers
NTRS | 1934
|Static thrust of airplane propellers
Engineering Index Backfile | 1932
|Static thrust of airplane propellers
TIBKAT | 1932
|Static thrust analysis for helicopter rotors and airplane propellers
Engineering Index Backfile | 1948
|Engineering Index Backfile | 1939
|