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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    Titel :

    Joining -- Real challenge in use of advanced structures


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Barker, W.T. (Autor:in)

    Kongress:

    SAE Meeting ; 1965 Fasteners



    Erscheinungsdatum :

    1965


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Joining, The Real Challenge in Use of Advanced Structures

    Barker, W. T. | SAE Technical Papers | 1965


    Cost The Challenge for Advanced Materials and Structures

    Davis, J. G. / Freeman, W. T. / Siddiqi, S. | British Library Online Contents | 1992



    Design guidelines for joining advanced composites

    Dreger,D.R. | Kraftfahrwesen | 1980


    Joining of P/M Structures

    Knopp, Walter V. | SAE Technical Papers | 1974