Logical combinations for these super-aluminum alloys are suggested that will be practical from production standpoint, yet result in strength-weight ratios for airplane structures. (See also Product Eng v 16 n 1 Jan 1945 p 6-11)


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    Title :

    High-strength aluminum alloys for lightweight structures


    Additional title:

    Automotive Aviation Industries


    Contributors:
    Tatman, N.E. (author) / Miller, R.A. (author)

    Published in:

    Publication date :

    1945


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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