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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    Title :

    Two-Dimensional Unsteady Incompressible Flow


    Contributors:


    Publication date :

    2024-06-11


    Size :

    22 pages




    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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