The unsteady aerodynamics is usually presented in terms of a relatively complicated integral equation where the unknown pressure jump appears within an integral over the wing system. This concept is introduced in this chapter.


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    Titel :

    Two-Dimensional Unsteady Incompressible Flow


    Beteiligte:


    Erscheinungsdatum :

    11.06.2024


    Format / Umfang :

    22 pages




    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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