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The geometry of the blade tip has a large impact on rotor performance. A modern double-swept tip geometry is experimentally compared to a standard reference geometry, with an emphasis on the evolution of the blade tip vortex.
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This page is a summary of: Tip Vortex Study of a Rotor with Double-Swept Blade Tips, AIAA Journal, May 2024, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j063426.
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