Aerodynamic characteristics of a joined wing were investigated by computational methods and by a low speed wind tunnel experiment for the purpose of understanding the aerodynamic characteristics and advantages of such a wing over conventional configurations, and to examine the feasibility of using it in a practical application. Extended lifting line theory, the three dimensional potential flow panel method, and the finite difference method were used.


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    Title :

    Computational and Experimental Analysis of Joined-Wing Aerodynamics


    Contributors:
    N. Hirose (author) / T. Ohnuki (author) / M. Hashimoto (author) / M. Ishikawa (author)

    Publication date :

    1990


    Size :

    23 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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