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This paper describes a generalized aircraft sizing and analysis framework intended for novel aircraft configurations and propulsion system architectures. Results are shown for an all-electric and a hybrid-electric variant of a ducted fan lift-plus-cruise VTOL aircraft.

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This page is a summary of: Design and Sizing of an Electrified Lift-Plus-Cruise Ducted Fan Aircraft, Journal of Aircraft, November 2022, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c036811.
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