Results of tests on extruded section of 27St aluminum alloy; loading continued until definite maximum value was reached.


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    Title :

    Lateral stability of equal-flanged aluminum alloy I-beams subjected to pure bending


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Notes


    Contributors:
    Dumont, C. (author) / Hill, H.N. (author)


    Publication date :

    1940


    Size :

    14 pages


    Remarks:

    11 Supp plates, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :



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