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of hybrid-electric aero-engine performance and environmental impact will be a key focus. The project also includes preliminary system design and mission analysis. A large part of the work will be conducted
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validation. You will be joining a strong team that works within the following domains: Dynamic turbine response modelling in the multi-body framework HAWC2 Aero-servo-hydro-elastic stability analysis
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industrial and academic partners. The work constitutes an integral part of research activities within several projects on flight electrification at FEC. Modelling and simulation of hybrid-electric aero-engine
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and validation. You will be joining a strong team that works within the following domains: Dynamic turbine response modelling in the multi-body framework HAWC2 Aero-servo-hydro-elastic stability
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simulation numérique avancée du phénomène hélicoptère Tail-Shake. 2022. Thèse de doctorat. Sorbonne Université. doi: tel-03850713v1 [3] http://www.prolb-cfd.com/research-and-development/ . CLIMB: Computational