What is it about?
In this paper, we optimize distributed electric propulsion aircraft using a holistic approach that examines vehicle performance over the entire mission rather than one design point. This approach is better suited for novel urban air mobility aircraft whose flight segments are comparable in duration.
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This page is a summary of: Aerodynamic Optimization of Wing-Mounted Propeller Configurations for Distributed Electric Propulsion Architectures, July 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/6.2021-2471.
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