Problem in analysis of aircraft structures is determination of buckling load of column supported at points along its span by other structural members; solution presented; charts, which relate deflectional spring stiffness, rotational spring stiffness, and buckling load, given for columns having two, three, four, and infinite number of spans.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Buckling of column on equally spaced deflectional and rotational springs


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1948


    Size :

    42 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English




    The buckling of a column on equally spaced deflectional and rotational springs

    Budiansky, Bernard / Seide, Paul / Weinberger, Robert A. | TIBKAT | 1948


    Buckling of a Column on Equally Spaced Deflectional and Rotational Springs

    B. Budiansky / P. Seide / R. A. Weinberger | NTIS | 1948




    Elliptic Displaced Orbit Approximation with Equally Spaced Impulses

    Caruso, Andrea / Mengali, Giovanni / Quarta, Alessandro A. | AIAA | 2019