Suggests method of calculation based on assumption that deformation of fuselage is due to stretch of panel bracing wires, bulkhead bracing wires being considered as inoperative.


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    Title :

    Torsional loads in the fuselage of an aeroplane


    Additional title:

    Engineering


    Contributors:

    Published in:

    Engineering ; 107 , n 2772


    Publication date :

    1919


    Remarks:

    1 Fig.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Torsional stresses in the fuselage of an aeroplane

    Pippard, Alfred John Sutton ;Douglas, W. D. | SLUB | 1921


    Torsional stresses in the fuselage of an aeroplane

    Pippard, Alfred John Sutton / Douglas, W. D. | TIBKAT | 1921