IN the following, the free flexional oscillations of a monoplane's semi-cantilever wing are given, taking into consideration the inner and outer parts of the strut as two systems coupled by elasticity. The result, which is identical with coupled electrical circuits, has been checked by tests with a light aeroplane.


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    Titel :

    Semi-Cantilever Wings


    Untertitel :

    A Mathematical Analysis, Checked by Experimental Tests, of the Free Oscillations in the System


    Beteiligte:
    Pasqualini, C. (Autor:in) / Biro, D. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.11.1935


    Format / Umfang :

    13 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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