Mass, primary energy, and cost: the impact of optimization objectives on the initial sizing of hybrid-electric general aviation aircraft
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DOI: 10.1007/s13272-020-00449-8
Abstract: For short take-off and landing (STOL) aircraft, a parallel hybrid-electric propulsion system potentially offers superior performance compared to a conventional propulsion system, because the short-take-off power requirement is much higher than the cruise power requirement.… read more here.
Keywords: methodology; general aviation; aircraft; initial sizing ... See more keywords