Calculated Spanwise Lift Distributions and Aerodynamic Influence Coefficients for Unswept Wings in Subsonic Flow.


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    Title :

    Calculated spanwise lift distributions and aerodynamic influence coefficients for unswept wings in subsonic flow


    Additional title:

    NACA -- Tech Note


    Contributors:


    Publication date :

    1953


    Size :

    120 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :