The Kutta conditionKutta condition in all physical and mathematical flow models defined in Sect. 10.1007/978-3-662-61328-3_1 is generally understood as appearing at acute edges of aerodynamic surfaces. That can be the “zero thickness” trailing edge of a large Aspect ratiolarge aspect-ratio wing or the “sharp” leading edge of a delta wing. Usually it is assumed that the flow leaves the trailing edge in bisector direction.


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    Title :

    About the Kutta Condition




    Publication date :

    2020-10-05


    Size :

    19 pages




    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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    Resolution of Runge-Kutta-Nystrom condition equations through eighthorder

    BATTIN, R. H. / MIT, Cambridge / Mass. | AIAA | 1976