The expression of the aerodynamic force previously obtained in Chap. 12 is used to derive the Kutta-Jukowsky Theorem for a two-dimensional wing. The boundary condition and Kutta’s condition are also presented. The case of flat plate and its implications on the Doublet Lattice Method are discussed.


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    Title :

    Theoretical Aerodynamic Modeling of Wings


    Contributors:


    Publication date :

    2024-06-11


    Size :

    20 pages




    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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