Procedure for case of simultaneous change of moment of inertia, change of distributed load, and concentrated load at point in main bay. (supp.)


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    Title :

    Graphical method of stressing aeroplane spars


    Additional title:

    Flight


    Contributors:

    Published in:

    Flight ; 23 , n 17


    Publication date :

    1931


    Remarks:

    7 Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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