Investigation of hinge moments of ailerons of various chords and spans on two airfoils having Clark Y and U.S.A. 27 wing sections in 10-ft. tunnel of Bureau of Standards on models of 60 in. span and 10 in. chord.


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    Title :

    Effect of variation of chord and span of ailerons on hinge moments at several angles of pitch


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1930


    Size :

    15 pages


    Remarks:

    30 Figs.


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English