Desirability of expanding airplane regulations to include proof of safety for unsymmetrical loading, at least in structural members specially stressed; flight cases involve increases of customary load assumptions through yawing and rolling moments; corresponding increases in their magnitude can be found; stresses particularly great in case of one-sided landing shock, because principal part of total inertia of plane lies in wings. From Zeit. fuer Flugtechnik und Motorluftschiffahrt, June 14, 1929.


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    Title :

    Unsymmetrical forces in an airplane cell


    Additional title:

    Nat. Advisory Committee Aeronautics -- Tech. Memo


    Contributors:
    Vogt, R. (author)


    Publication date :

    1929


    Size :

    9 pages


    Remarks:

    4 Figs.


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :




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