Recent efforts in extreme short takeoff and landing aircraft configurations have renewed the interest in circulation control wing design and optimization. The key to accurately designing and optimizing these configurations rests in the modeling of the complex physics of these flows. This paper will highlight the physics of the stagnation and separation regions on two typical circulation control airfoil sections.


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    Titel :

    Experimental Investigation of a 2D Supercritical Circulation-Control Airfoil Using Particle Image Velocimetry


    Beteiligte:

    Kongress:

    3rd AIAA Flow Control Conference ; 2006 ; San Francisco, CA, United States


    Erscheinungsdatum :

    01.01.2006


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch





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