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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    Title :

    Materials for Aircraft Structures


    Contributors:

    Published in:

    Publication date :

    1950-05-01


    Size :

    7 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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