Dimensional analysis leading to derivation of deflection formula for beams of constant section of types commonly encountered in airplane design; tables and curves of non-dimensional coefficients; variation of spring constant with changes in axial load and position along beam.


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    Title :

    Deflection formula for single-span beams of constant section subjected to combined axial and transverse loads


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Notes


    Contributors:
    Burke, W.F. (author)


    Publication date :

    1935


    Remarks:

    21 Supp sheets, Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



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    Note on beams under combined side and axial loads

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