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Electric, hybrid, and turboelectric fixed-wing aircraft

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Electric, hybrid, and turboelectric fixed-wing aircraft ( electric-hybrid-and-turboelectric-fixed-wing-aircraft )

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[92] M. J. Armstrong, C. A. H. Ross, M. J. Blackwelder, Propulsion System Com- ponent Considerations for NASA N3-X Turboelectric Distributed Propulsion System, SAE International Journal of Aerospace 5 (2) (2012) 344–353. doi: 10.4271/2012-01-2165. [93] C. Ross, M. Armstrong, M. Blackwelder, C. Jones, P. Norman, S. Fletcher, Tur- boelectric Distributed Propulsion Protection System Design Trades, SAE Tech- nical Paper 2014-01-2141doi:10.4271/2014-01-2141. [94] J. C. Shaw, P. Norman, S. Galloway, G. Burt, A Method for the Evalua- tion of the Effectiveness of Turboelectric Distributed Propulsion Power Sys- tem Architectures, SAE International Journal of Aerospace 7 (1) (2014) 35–43. doi:10.4271/2014-01-2120. [95] K. Davies, P. Norman, C. Jones, S. Galloway, G. Burt, Modelling the Fault Behaviour of a Superconducting Turboelectric Distributed Propulsion Network Overview of Superconducting DC Networks, SAE Technical Paper 2014-01- 2142doi:10.4271/2014-01-2142. [96] J. C. Shaw, S. Fletcher, P. Norman, S. Galloway, G. Burt, Failure Analysis of a Turboelectric Distributed Propulsion Aircraft Electrical Network : A Case Study, SAE Technical Paper 2015-01-2403doi:10.4271/2015-01-2403. [97] K. R. Antcliff, F. M. Capristan, Conceptual Design of the Parallel Electric-Gas Architecture with Synergistic Utilization Scheme (PEGASUS) Concept, in: 18th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Denver, CO, 2017. doi:10.2514/6.2017-4001. [98] F. Berg, J. Palmer, P. Miller, M. Husband, G. Dodds, HTS electrical system for a distributed propulsion aircraft, IEEE Transactions on Applied Superconductivity 25 (3). doi:10.1109/TASC.2014.2384731. [99] F. Berg, J. Palmer, L. Bertola, P. Miller, G. Dodds, Cryogenic system options for a superconducting aircraft propulsion system, IOP Conference Series: Materials Science and Engineering 101 (1). doi:10.1088/1757-899X/101/1/012085. [100] F. Berg, J. Palmer, P. Miller, G. Dodds, HTS System and Component Targets for a Distributed Aircraft Propulsion System, IEEE Transactions on Applied Superconductivity 27 (4). doi:10.1109/TASC.2017.2652319. [101] K. Smith, This LA company is developing all- electric , zero-emission airplane, Los Angeles Daily News (November 2017). URL http://www.dailynews.com/2017/11/07/ this-la-company-is-developing-all-electric-zero-emission-airplane/ [102] M. Kreimeier, E. Stumpf, Benefit evaluation of hybrid electric propulsion con- cepts for CS-23 aircraft, CEAS Aeronautical Journal 8 (4) (2017) 691–704. doi:10.1007/s13272-017-0269-9. 46

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