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Propellers used for electric vertical takeoff and landing (eVTOL) aircraft propulsion systems experience a wide range of aerodynamic conditions, including large incidence angles relative to oncoming airflow. This paper describes a novel mathematical model development methodology for propellers operating at high incidence angles.
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This page is a summary of: System Identification for Propellers at High Incidence Angles, Journal of Aircraft, July 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c036329.
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