Effect of ailerons quantitatively investigated on basis of Prandtl's wing theory; angle of attack increased at one end and decreased at other; distribution of circulation expressed by Fourier series; distribution calculated for different aileron lengths; rolling moment, additional induced drag and yawing moment determined from distribution; relations when both ailerons are deflected in same direction. From Tokyo Imperial University -- Report of Aeronautical Research Inst., Dec. 1927.


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    Title :

    Theoretical investigation of the effect of the Ailerons on the wing of an airplane


    Additional title:

    Nat. Advisory Committee Aeronautics -- Tech. Mem


    Contributors:


    Publication date :

    1929


    Size :

    25 pages


    Remarks:

    4 Figs.


    Type of media :

    Book


    Type of material :

    Print


    Language :

    English