Mathematical theory of stability of fuselage subjected to torsional force in case of light-metal airplane in flight; experimental check of theory by testing india-rubber cylindrical shells of various thicknesses and lengths twisted by special apparatus.


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    Title :

    Nature of torsional stability of monocoque fuselage


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:
    Sezawa, K. (author)

    Published in:

    Publication date :

    1933


    Size :

    12 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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