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Most battery-driven urban air mobility (UAM) vehicles have been restricted the range to intracity operation by the battery technology limitations. To this end, we propose a generic design methodology for designing vertical take-off and landing aircraft with a hybrid-electric propulsion system as an alternative to facilitate intercity missions for urban air mobility.

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This page is a summary of: Generic Design Methodology for Vertical Takeoff and Landing Aircraft with Hybrid-Electric Propulsion, Journal of Aircraft, September 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c036214.
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