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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    Titel :

    Design of spot welded aluminum alloy aircraft structures


    Weitere Titelangaben:

    Aero Digest


    Beteiligte:
    Epstein, A. (Autor:in) / Klinke, H.O. (Autor:in)

    Erschienen in:

    Aero Digest ; 45 , n 1


    Erscheinungsdatum :

    1944


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Fatigue Design of Welded Aluminum Structures

    Menzemer, Craig C. | Online Contents | 1993



    Mechanical and corrosion tests of spot-welded aluminum alloys

    Reinhart, F.M. / Hess, W.F. / Wyant, R.A. et al. | Engineering Index Backfile | 1951