Design formula for torsional vibration of conically tapered shell fixed at one end and carrying mass of appreciable moment of inertia at free end. (supp)


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    Title :

    Fuselage stiffness


    Additional title:

    Flight


    Contributors:
    Morris, J. (author)

    Published in:

    Flight ; 30 , n 1457


    Publication date :

    1936


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English






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