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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    Title :

    Semi-Cantilever Wings


    Subtitle :

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


    Contributors:
    Pasqualini, C. (author) / Biro, D. (author)

    Published in:

    Publication date :

    1935-11-01


    Size :

    13 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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