Improvements in current methods for calculation of loads in members of metal-truss wing spars subjected to combined bending and compression; effective moment of inertia of actual metal-truss wing spar is calculated for wing spar built and tested by Boeing Airplane Co.; calculated value is checked against test data, and conclusions are drawn regarding accuracy of calculated value.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Metal-truss wing spars


    Additional title:

    Nat. Advisory Committee Aeronautics -- Tech. Notes


    Contributors:


    Publication date :

    1931


    Size :

    31 pages


    Remarks:

    9 Figs., Supp. plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Metal-truss wing spars

    Swickard, Andrew E | NTRS | 1931


    Metal truss wing spars

    Swickard, Andrew E. | SLUB | 1931


    Metal wing spars

    Engineering Index Backfile | 1927


    Calculation of wing spars

    Ratzersdorfer, Julius | NTRS | 1921