Simple method for designing propeller for given arrangement of airplane parts; inflow to propeller and efficiency of propeller affected most by fuselage; flow conditions in plane of propeller, which are affected by shape of fuselage; determined mathematically; condition for best thrust distribution; induced efficiency of propeller calculated. (see also Nat. Advisory Committee for Aeronuatics -- Tech. Memorandums, No. 492, Dec. 1928, 11 pp., 5 figs. on supp. page.)
Effect of fuselage on design of aircraft propellers
Zur Beruecksichtigung des Rumpfers beim Luftschraubenentwurf
1928
5 pages
5 Figs.
Article (Journal)
German
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