Publications

• S. Mezani, et al., Performances of direct drive and magnetically geared PMSMs with different cooling technologies, Intermag2024, DOI: 10.5281/zenodo.12580005, link
• H. Kellermann, Design of Thermal Management Systems for Future Aircraft, Thesis, URN: details, link
• D. Keller et al., Aerodynamic Investigation of a Propeller-Driven Transport Aircraft with Distributed Propulsion within the Imothep Project, ECCOMAS 2024, link
• E. Nguyen Van et al., Design and performances of a turbo-electric and Distributed Propulsion aircraft in the Small and Medium Range segment: intermediate results from the European project IMOTHEP, AIAA 2024 SciTech, link
• Ph. Novelli, Perspectives of hybridization for commercial aircraft: the lessons learned from the IMOTHEP project: Keynote, MEA2024, link
• J. van Muijden et al, First order thermal analysis methodology for hybrid-electric propelled aircraft in early design stages, 10ᵀᴴ EUCASS/9ᵀᴴ CEAS, DOI: 10.13009/EUCASS2023-375, link
• S. Guerin et al, A contribution to the investigation of acoustic interferences in aircraft distributed propulsion, CEAS Aeronautical Journal (2023) 14:965-982, DOI: https://doi.org/10.1007/s13272-023-00679-6, link
• Ph Novelli, et al., IMOTHEP: toward a roadmap for the development of hybrid electric propulsion, Joint IMOTHEP/ CAJU Workshop 2023, DOI: 10.5281/zenodo.10400474, link
• Ph Novelli, et al., IMOTHEP: toward a roadmap for the development of hybrid electric propulsion : Synthesis of results, Joint IMOTHEP/ CAJU Workshop 2023, DOI: 10.5281/zenodo.10400518, link
• Ph. Novelli et al, IMOTHEP European project: an investigation of hybrid electric propulsion for commercial aircraft, AIAA 2023 Aviation Forum, DOI: 10.2514/6.2023-4131, link 
• A.L. Habermann et al, Aerodynamic Effects of a Wing Surface Heat Exchanger, Aerospace 2023, 10(5), 407, DOI: https://doi.org/10.3390/aerospace10050407, link
• A.L. Habermann et al, Study of a Regional Turboprop Aircraft with Electrically Assisted Turboshaft, Aerospace 2023, 10(6), 529, https://doi.org/10.3390/aerospace10060529, link
• H. Kühnelt et al, Are batteries fit for hybrid-electric regional aircraft?, J. Phys.: Conf. Ser. 2526 (2023) 012026, DOI: 10.1088/1742-6596/2526/1/012026, link
• D. Keller, Aerodynamic Investigation of the High-Lift Performance of a Propeller-Driven Regional Transport Aircraft with Distributed Propulsion, J. Phys. Conf. Ser. 2526 (2023) 012007, DOI: 10.1088/1742-6596/2526/1/012007, link
• S. Mezani, et al., Electrical Machine with HTS winding: Analytical Design and Optimization, ISEF2023, DOI: 10.5281/zenodo.12592026, link
• Y. Laïb et al., Static characterization on-state of an industrial Si Power MOSFET at cryogenic temperature, EUCAS2023, DOI: 10.5281/zenodo.11509862, link
• T. Marcand et al., Multiphysics modeling and optimization of PMSM for high speed operation, Intermag2023, DOI: 10.5281/zenodo.12579817, link
• C. Viguier, Superconducting motor associated with a superconducting power train, EUCAS2023, DOI: 10.5281/zenodo.11517513, link
• D. Larbi et al., Design and Comparison of High-speeds PMSM and IM for Aircraft Application, DOI: 10.1109/ITECAsia-Pacific59272.2023.10372325, link
• S. Toghyani et al, Conceptual Design of Solid-State Li-Battery for Urban Air Mobility, J. Electrochem. Soc. 170 (2023) 103510, DOI: 10.1149/1945-7111/ad00de, link
• S. Toghyani et al, Model-Based Design of High Energy All-Solid-State Li Batteries with Hybrid Electrolytes, J. Electrochem. Soc. 169 (2022) 040550, DOI: 10.1149/1945-7111/ac653b, link
• R. Dorget, Superconducting motor associated with cryogenics power electronics for aircrafts, ASC'2022, DOI: 10.5281/zenodo.11516955, link
• J. Vankan et al, Conceptual design study for a radical short-medium range hybrid aircraft, 9th EUCASS 2022, DOI: 10.13009/EUCASS2022-4789, link
• J. van Muiden et al, Thermal management principal analysis of hybrid-electric aircraft with turboelectric propulsion using distributed propulsors, 9th EUCASS 2022, DOI: 10.13009/EUCASS2022-6103, link
• V. J. E. Aalbers et al, Low-fidelity Aerodynamic Integration of Distributed Electric Propulsion on a Blended Wing Body including Boundary Layer Ingestion, 9th EUCASS 2022, DOI:10.13009/EUCASS2022-6105, link 
• S. Mezani et al, Sizing Electrical Machines Using OpenOffice Calc, 9th EUCASS 2022, DOI: 10.13009/EUCASS2022-6110, link
• E. Nguyen Van et al, Design and performance evaluation of a full turboelectric distributed electric propulsion aircraft: Preliminary results of EU project IMOTHEP, 9th EUCASS 2022, DOI: 10.13009/EUCASS2022-6134, link
• J. Lévêque et al, Sizing Superconducting motor associated with cryogenics power electronics for disruptive hybrid electric propulsion aircrafts, 9th EUCASS 2022, DOI: 10.13009/EUCASS2022-7234, link
• V. Cesare et al, Power Management and Fault Analysis Hybrid Propulsion Aircraft System, 9th EUCASS 2022, DOI:10.13009/EUCASS2022-7313, link
• X. Zhao et al, Development of an aerodynamic analysis tool for boundary layer ingestion concept design, ICAS2022, link
• J. Gauvrit-Ledogar et al, Multidisciplinary Design and Optimization of the Blended Wing Body Configuration SMILE, 9th EUCASS 2022, DOI: 10.13009/EUCASS2022-6061, link
• Ph. Novelli, IMOTHEP: toward a roadmap for the development of hybrid electric propulsion, 12th EASN 2022, link
• S. Guerin et al, Parametric Study of the Noise Emitted by Uncorrelated, Distributed, Electric Fans, AIAA 2021 Aviation Forum, DOI: https://doi.org/10.2514/6.2021-2137, link
  

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