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Comparative Study of Hybrid Electric Distributed Propulsion Aircraft Through Multiple Powertrain Component Modeling Approaches

dc.contributor.authorBaptiste Legrand
dc.contributor.authorArnaud Gaillard
dc.contributor.authorDavid Bouquain
dc.contributor.otherUniversité Marie et Louis Pasteur, UTBM, CNRS, Institut FEMTO-ST, FCLAB, F-90000 Belfort, France
dc.contributor.otherUniversité Marie et Louis Pasteur, UTBM, CNRS, Institut FEMTO-ST, FCLAB, F-90000 Belfort, France
dc.contributor.otherUniversité Marie et Louis Pasteur, UTBM, CNRS, Institut FEMTO-ST, FCLAB, F-90000 Belfort, France
dc.date.accessioned2025-08-27T14:00:02Z
dc.date.accessioned2025-10-08T08:35:44Z
dc.date.available2025-10-08T08:35:44Z
dc.date.issued01-08-2025
dc.identifier.urihttp://digilib.fisipol.ugm.ac.id/repo/handle/15717717/36171
dc.description.abstractAircraft design is an ever-expanding field of research. Disruptive aircraft architectures and the long-standing need for fast design processes are the main drivers behind the domain growth. Novel concepts like distributed propulsion, Vertical Take-Off and Landing, electrification, hybridization, etc., require new models and design strategies to achieve a significant degree of fidelity at every stage of the design. This paper proposes a framework targeting key techniques and assumptions to improve the accuracy of the preliminary aircraft design stage. Based on a review of modern design strategies, a model-based method has been developed. Two distinct approaches to component modeling have been compared for a hybrid-electric distributed propulsion aircraft. To complement this comparative study, the second modeling approach has been tested for three different hybrid electric architectures. The results showcase the feasibility of the three architectures, with promising results for the hydrogen powertrain system.
dc.language.isoEN
dc.publisherMDPI AG
dc.subject.lccMotor vehicles. Aeronautics. Astronautics
dc.titleComparative Study of Hybrid Electric Distributed Propulsion Aircraft Through Multiple Powertrain Component Modeling Approaches
dc.typeArticle
dc.description.keywordsaircraft powertrain
dc.description.keywordsdistributed propulsion aircraft
dc.description.keywordshybrid propulsion
dc.description.keywordshydrogen aircraft
dc.description.keywordsaircraft design
dc.description.keywordscomponent modeling
dc.description.doi10.3390/aerospace12080732
dc.title.journalAerospace
dc.identifier.e-issn2226-4310
dc.identifier.oaioai:doaj.org/journal:af7aadc202f8434597c502cd9bfd2036
dc.journal.infoVolume 12, Issue 8


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