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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[147] [148] [149] [150] [151] [152] [153] [154] [155] [156] [157] C. E. Jones, P. J. Norman, S. J. Galloway, M. J. Armstrong, A. M. Bollman, Comparison of candidate architectures for future distributed propulsion aircraft, IEEE Transactions on Applied Superconductivity 26 (6) (2016) 1–9. doi:10. 1109/TASC.2016.2530696. G. Warwick, NASA Moves Electric-Propulsion Components Closer To Reality, Aviation Week (2017). URL http://aviationweek.com/commercial-aviation/ nasa-moves-electric-propulsion-components-closer-reality S. Trimble, GE reveals major achievements in hybrid electric propulsion, Flight- Global (August 2017). S. Trimble, ANALYSIS : Key challenges in the race to develop hybrid-electric aircraft, FlightGlobal (November 2017). C. E. Lents, L. W. Hardin, J. Rheaume, L. Kohlman, Parallel Hybrid Gas- Electric Geared Turbofan Engine Conceptual Design and Benefits Analysis, in: 52nd AIAA/SAE/ASEE Joint Propulsion Conference, Salt Lake City, UT, 2016. doi:10.2514/6.2016-4610. R. H. Jansen, C. Bowman, A. Jankovsky, Sizing Power Components of an Elec- trically Driven Tail Cone Thruster and a Range Extender, in: 16th AIAA Avia- tion Technology, Integration, and Operations Conference, Washington, DC, 2016. doi:10.2514/6.2016-3766. S. L. Schnulo, J. Chin, A. D. Smith, A. Dubois, Steady State Thermal Analyses of SCEPTOR X-57 Wingtip Propulsion, in: 17th AIAA Aviation Technology, Integration, and Operations Conference, Denver, CO, 2017, pp. 1–14. doi:10. 2514/6.2017-3783. J. C. Gladin, D. Trawick, C. A. Perullo, J. C. Tai, D. N. Mavris, Modeling and Design of a Partially Electric Distributed Aircraft Propulsion System with GT- HEAT, in: 55th AIAA Aerospace Sciences Meeting, Grapevine, TX, 2017, pp. 1–18. doi:10.2514/6.2017-1924. J. C. Gladin, C. A. Perullo, J. C. Tai, D. N. Mavris, A Parametric Study of Hybrid Electric Gas Turbine Propulsion as a Function of Aircraft Size Class and Technology Level, in: 55th AIAA Aerospace Sciences Meeting, Grapevine, TX, 2017. doi:10.2514/6.2017-0338. F. M. Capristan, J. R. Welstead, An Energy-Based Low-Order Approach for Mission Analysis of Air Vehicles in LEAPS, in: 2018 AIAA Aerospace Sciences Meeting, Kissimmee, FL, 2018. doi:10.2514/6.2018-1755. J. R. Welstead, D. Caldwell, R. Condotta, N. Monroe, An Overview of the Layered and Extensible Aircraft Performance System (LEAPS) Development, in: 2018 AIAA Aerospace Sciences Meeting, Kissimmee, FL, 2018. doi: 10.2514/6.2018-1754. 51

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