Theoretical mathematical analysis of distribution of lift along fuselage with axial and diagonal flow, and influence of downwash on tail unit, in case of monoplane with wing midway up fuselage of symmetrical revolution, with having infinite span and constant circulation; distribution of lift about wing for case of spherical fuselage.


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    Title :

    Zur theoretischen Behandlung des gegenseitigen einflusses von Tragfluegel und Rumpf


    Additional title:

    Zur theoretischen Behandlung des gegenseitigen einflusses von Tragfluegel und Rumpf


    Contributors:
    Vandrey, F. (author)

    Published in:

    Publication date :

    1937


    Size :

    9 pages


    Remarks:

    Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    German