Suitability of existing materials; it is shown that hypothetical material derived by expanding aluminum alloy would greatly simplify structure of fuselages.


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    Title :

    Materials for aircraft structures


    Additional title:

    Aircraft Eng


    Contributors:

    Published in:

    Publication date :

    1950


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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