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An energy-based aircraft sizing framework and methodology is used to demonstrate sizing of a vertical takeoff and landing tilt-wing urban air mobility aircraft with all-electric and hybrid-electric propulsion systems.
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This page is a summary of: Sizing of Tilt-Wing Aircraft with All-Electric and Hybrid-Electric Propulsion, Journal of Aircraft, August 2022, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c036813.
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