Aerodynamic study of a leading-edge rotating cylinder in a cambered aerofoil (NACA2412)

What is it about?

The aviation industry faces challenges in flow separation over the wing, which can lead to stall effects and increased drag. To address this, active flow control methods like the Moving Surface Boundary (MSB) technique are used to introduce momentum into shear flow. This paper discusses the effectiveness of MSB in the NACA 2412 aerofoil shape.

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