Numerical results for coefficients of system where aileron hinge axis coincides with nose of aileron; complete set of 5 complex coefficients is given for Mach numbers 0, 0.35, 0.50, 0.60, 0.70, 0. 80, reduced frequency being equal to 0 (0.1) 1.0 and chord ratio equal to 0 (0.02) 0.1 (0.05) 0.3.


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    Title :

    Tables of aerodynamic aileron-coefficients for oscillating wing-aileron system in subsonic, compressible flow


    Additional title:

    Amsterdam Nationaal Luchtvaartlaboratorium (Nat Aeronautical Research Inst) -- Report


    Contributors:


    Publication date :

    1954


    Size :

    21 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :






    Aircraft wing with aileron

    MARK SHAUN KELLY / STUART ALEXANDER | European Patent Office | 2018

    Free access