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RISEffect of a Single Leading-Edge Protuberance on NACA 634-021 Airfoil Performance
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Effect of a Single Leading-Edge Protuberance on NACA 634-021 Airfoil Performance;Leading-edge protuberances on airfoils or wings have been considered as a viable passive control method for flow separation. In this paper, ...