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.
Experimental Investigation of a 2D Supercritical Circulation-Control Airfoil Using Particle Image Velocimetry
3rd AIAA Flow Control Conference ; 2006 ; San Francisco, CA, United States
2006-01-01
Conference paper
No indication
English
British Library Conference Proceedings | 2006
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