Phase concerning relation of physical properties of spot welds to type of loads and service conditions experienced in aircraft has been given little attention; paper attempts to cover this phase with particular reference to primary structure of airplane; general review of factors that have limited use of spot welding in primary structure in past is included. (See also - v 44 n 3 Feb 1 1944 p 80, 84, 204, 207, 209-10, 214, n 5 Mar 1 p 121, 123, 125, 194, 196, 199)


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    Title :

    Design of spot welded aluminum alloy aircraft structures


    Additional title:

    Aero Digest


    Contributors:
    Epstein, A. (author) / Klinke, H.O. (author)

    Published in:

    Aero Digest ; 45 , n 1


    Publication date :

    1944


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English





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