Methods are here given for ascertaining the value of n in Euler's simplified formula, P = n (EI/l(sup 2)), for the compressive strength of tapered airplane struts, by estimating from curves and by calculation.


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    Title :

    Compressive Strength of Tapered Airplane Struts


    Contributors:

    Publication date :

    1923-12-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Compressive strength of tapered airplane struts

    Lewe, Viktor | Engineering Index Backfile | 1923


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    Teichmann, A. | Engineering Index Backfile | 1930