Methods for ascertaining value of n in Euler's simplified formula for compressive strength of tapered airplane struts, by estimating from curves and by calculation. Translated from Technische Berichte, vol. 3, no. 7.


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    Title :

    Compressive strength of tapered airplane struts


    Additional title:

    U. S. Nat. Advisory Committee Aeronautics, Technical Notes


    Contributors:


    Publication date :

    1923


    Size :

    8 pages


    Remarks:

    1 Fig.


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :



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