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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    Titel :

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


    Weitere Titelangaben:

    Nat. Advisory Committee Aeronautics -- Tech. Mem


    Beteiligte:


    Erscheinungsdatum :

    1929


    Format / Umfang :

    25 pages


    Anmerkungen:

    4 Figs.


    Medientyp :

    Buch


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :