In this article the author discusses the suitability of existing materials for aircraft structures and shows that a hypothetical material derived by expanding an aluminium alloy would greatly simplify the structure of fuselages


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    Titel :

    Materials for Aircraft Structures


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    01.05.1950


    Format / Umfang :

    7 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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