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.)


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    Title :

    Effect of fuselage on design of aircraft propellers


    Additional title:

    Zur Beruecksichtigung des Rumpfers beim Luftschraubenentwurf


    Contributors:
    Troller, T. (author)


    Publication date :

    1928


    Size :

    5 pages


    Remarks:

    5 Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    German




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