Investigation carried out in 5-ft. wind tunnel of Langley Memorial Aeronautical Laboratory for purpose of obtaining more complete information than was heretofore available on distribution of lift between ends of wing spars, stresses in ailerons, and general subject of air flow near tip of wing.


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    Title :

    The distribution of lift over wing tips and ailerons


    Additional title:

    U. S. Nat. Advisory Committee Aeronautics. Report


    Contributors:


    Publication date :

    1923


    Size :

    24 pages


    Remarks:

    29 Figs.


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :