Method of attachment and effects of joining method are of equal importance to selection of materials; joining design problems arising from inadequate consideration of practical factors are shown; examples are given ranging from WW II aircraft (collection of holes held together with fasteners) to space vehicles' fastening system; examples relate to re-entry body test structure requiring use of multilayered construction, joining problem involving cryogenic temperature, and heat sink leading edge attachment of X-15 aircraft.


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    Title :

    Joining -- Real challenge in use of advanced structures


    Additional title:

    SAE -- Paper


    Contributors:

    Conference:

    SAE Meeting ; 1965 Fasteners



    Publication date :

    1965


    Size :

    9 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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