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.


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    Titel :

    Study of unsymmetrical-loading conditions


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Pearson, H.A. (Autor:in)


    Erscheinungsdatum :

    1940


    Format / Umfang :

    34 pages


    Anmerkungen:

    12 Supp sheets, Bibliography


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    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