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We show novel enhancements to the electric propulsion system analysis method for electric vertical takeoff and landing (eVTOL) aircraft conceptual design by considering the electrical characteristics of each electrical device in a more accurate manner.
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This page is a summary of: Novel Electric Propulsion System Analysis Method for Electric Vertical Takeoff and Landing Aircraft Conceptual Design, Journal of Aircraft, January 2024, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c037225.
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