Comparative Assessment of Parallel-Hybrid-Electric Propulsion Systems for Four Different Aircraft
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[1] Daniel Raymer. Vehicle scaling laws for multidisciplinary optimization (Preliminary report) , 2001 .
[2] Cees Bil,et al. Initial Sizing Methodology for Hybrid-Electric General Aviation Aircraft , 2020 .
[3] Snorri Gudmundsson. The Aircraft Design Process , 2014 .
[4] Phillip J. Ansell,et al. Mission Analysis and Component-Level Sensitivity Study of Hybrid-Electric General-Aviation Propulsion Systems , 2018 .
[5] Andrew R. Gibson,et al. Design and Performance of the NASA SCEPTOR Distributed Electric Propulsion Flight Demonstrator , 2016 .
[6] Steven R.H. Barrett,et al. Technical and environmental assessment of all-electric 180-passenger commercial aircraft , 2019, Progress in Aerospace Sciences.
[7] D. Felix Finger,et al. Case Studies in Initial Sizing for Hybrid-Electric General Aviation Aircraft , 2018, 2018 AIAA/IEEE Electric Aircraft Technologies Symposium (EATS).
[8] Roelof Vos,et al. Preliminary Sizing of a Hybrid-Electric Passenger Aircraft Featuring Over-the-Wing Distributed-Propulsion , 2019 .
[9] I. H. Rettie,et al. Role of Figures of Merit in Design Optimization and Technology Assessment , 1981 .
[10] Daniel Raymer,et al. Aircraft Design: A Conceptual Approach, Sixth Edition , 2012 .
[11] C Bil,et al. On the Applicability of Empirical Drag Estimation Methods for Unmanned Air Vehicle Design , 2018, 2018 Aviation Technology, Integration, and Operations Conference.
[12] Leo L. Veldhuis,et al. Aerodynamic Investigation of an Over-the-Wing Propeller for Distributed Propulsion , 2018 .
[13] Mark D. Moore,et al. Misconceptions of Electric Aircraft and their Emerging Aviation Markets , 2014 .