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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    Titel :

    Theoretical Aerodynamic Modeling of Wings


    Beteiligte:


    Erscheinungsdatum :

    11.06.2024


    Format / Umfang :

    20 pages




    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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