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Hybrid electric aircraft is more and more a reality, since the main needing for the upcoming years is the reduction of emissions. This paper shows a multidisciplinary framework for the hybrid electric aicraft optimization.

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This page is a summary of: Multidisciplinary Design Optimization Framework with Coupled Derivative Computation for Hybrid Aircraft, Journal of Aircraft, July 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c035509.
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