Force variation along wing span under combined normal and angular accelerations considered; required aerodynamic load distributions obtained by use of wing theory and wing inertia distributions are based on analysis of wing weight data; several examples included to illustrate effect of wing taper and aileron span on total shears and moments at any section along span.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Study of unsymmetrical-loading conditions


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1940


    Size :

    34 pages


    Remarks:

    12 Supp sheets, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    A study of unsymmetrical-loading conditions

    Pearson, Henry A. | TIBKAT | 1940


    Stresses in Streamline Shells Due to Unsymmetrical Loading

    Binnie, A.M. | Emerald Group Publishing | 1947



    Unsymmetrical locomotive

    Koffman, J.L. | Engineering Index Backfile | 1962


    Unsymmetrical Catamarans

    Soding, H. / Technical University of Wroclaw | British Library Conference Proceedings | 1997