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Cycloidal rotors are a new vertical takeoff and landing flight system currently being implemented onto unmanned aerial vehicles and micro aerial vehicles. In this study, we investigate the blade tip vortices created by cycloidal rotors and their effect on lift generation.

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This page is a summary of: Cycloidal Rotor-Blade Tip-Vortex Analysis at Low Reynolds Number, AIAA Journal, June 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j058207.
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