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Coaxial, counter-rotating rotor systems are prone to high vibration due to the interaction of upper and lower rotor blades. This study explores a combined experimental-numerical methodology to investigate the source of these transient loads.

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This page is a summary of: Blade Passage Loads and Deformation of a Coaxial Rotor System in Hover, Journal of Aircraft, November 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c035469.
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