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Circulation control airfoils use a clever trick from fluid dynamics—the Coanda effect—to steer or lift an aircraft without traditional moving parts like flaps or rudders. In this study, we discovered that as high-speed air is blown over the curved trailing edge of such an airfoil, it naturally sheds large swirling vortices near the exit slot. These vortices stir up the surrounding airflow, causing the jet to lose energy faster than desired and reducing control effectiveness. By slightly lowering a small lip at the jet exit, we can shrink these vortices, slow down the jet’s energy loss, and significantly improve performance. This insight helps engineers design simpler, more efficient “rudderless” aircraft that rely on airflow alone for control—making them lighter, quieter, and more reliable.

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This page is a summary of: Characteristics of the shedding vortex around the Coanda surface and its impact on circulation control airfoil performance, Physics of Fluids, February 2023, American Institute of Physics,
DOI: 10.1063/5.0139806.
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