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Aerospace 2018, 5, 123 20 of 21 References 1. ICAO Enviromental Report 2010 Aviation and Climate Change. Available online: https://www.icao.int/ environmental-protection/Documents/Publications/ENV_Report_2010.pdf (accessed on 31 October 2018). 2. Advisory Council for Aeronautical Research in Europe (ACARE). European Aeronautics: A Vision for 2020. Available online: https://www.acare4europe.org/sites/acare4europe.org/files/document/Vision%202020_ 0.pdf (accessed on 31 October 2018). 3. Pornet, C.; Isikveren, A.T. Conceptual design of hybrid-electric transport aircraft. Prog. Aerosp. Sci. 2015, 79, 114–135. [CrossRef] 4. Cameretti, M.C.; Del Pizzo, A.; Di Noia, L.P.; Ferrara, M. Preliminary analysis of Hybrid-Electric propulsion system integrated in a regional aircraft. In Proceedings of the AEIT Congress, Bari, Italy, 3–5 October 2018. 5. Frosina, E.; Senatore, A.; Palumbo, L.; Di Lorenzo, G.; Pascarella, C. Development of a lumped parameter model for an aeronautic hybrid-electric propulsion system. Aerosp. J. 2018, 5, 105. [CrossRef] 6. Frosina, E.; Senatore, A.; Caputo, C.; Marinaro, G.; Di Lorenzo, G.; Pascarella, C. Modelling of a hybrid-electric light aircraft. Energy Proced. 2017, 126, 1155–1162. [CrossRef] 7. Perullo, C.; Mavris, D. A review of hybrid-electric energy management and its inclusion in vehicle sizing. Aircraft Eng. Aerosp. Technol. 2014, 86, 550–557. [CrossRef] 8. Friedrich, C.; Robertson, P.A. Hybrid electric-propulsion for automotive and aviation applications. CEAS Aeronaut. J. 2015, 6, 279–290. [CrossRef] 9. Pornet, C.; Kaiser, S.; Isikveren, A.T.; Hornung, M. Integrated fuel-battery hybrid for a narrow-body sized transport aircraft. Aircraft Eng. Aerosp. Technol. 2014, 86, 568–574. [CrossRef] 10. Müller, C.; Kieckhäfer, K.; Spengler, T.S. The influence of emission thresholds and retrofit options on airline fleet planning: An optimization approach. Energy Policy J. 2017. [CrossRef] 11. Baharozu, E.; Soykan, G.; Baris Ozerdem, M. Future aircraft concept in terms of energy efficiency and environmental factors. Energy 2017, 140, 1368–1377. [CrossRef] 12. Thauvin, J.; Barraud, G.; Roboam, X.; Sareni, B.; Budinger, M.; Leray, D. Hybrid propulsion for regional aircraft: A comparative analysis based on energy efficiency. In Proceedings of the ESARS-ITEC 2016, Toulouse, France, 2–4 November 2016. 13. Friedrich, C.; Robertson, P.A. Hybrid-electric propulsion for aircraft. J. Aircr. 2015, 52, 176–189. [CrossRef] 14. Gladin, J.; Trawick, D.; Perullo, C.; Tai, J.C.M.; Mavris, D.N. Modeling and design of a Partially electric distributed aircraft propulsion system with GT-HEAT. In Proceedings of the 55th AIAA Aerospace Sciences Meeting, Grapevine, TX, USA, 9–13 January 2017. 15. Lenssen, R.H. Series Hybrid Electric Aircraft: Comparing the Well-to-Propeller Efficiency with a Conventional Propeller Aircraft. Master’s Thesis, Delft University of Technology, Delft, The Netherlands, 2016. 16. Seitz, A.; Schmitz, O.; Isikveren, A.T.; Hornung, M. Electrically powered propulsion: Comparison and contrast to gas turbines. In Proceedings of the Deutscher Luft- und Raumfahrtkongress 2012, Berlin, Germany, 10–12 September 2012. ID: 281358. 17. Bradley, M.; Droney, C.; Gowda, S.; Kirby, M.; Paisley, D.; Roth, B. NASA N+3 Subsonic Ultra Green Aircraft Research SUGAR Final Review; Boeing Research and Technology Presentation, Boeing Airplane Company; NASA: Washington, DC, USA, 2010. 18. Masson, P.J.; Brown, G.V.; Soban, D.S.; Luongo, C.A. HTS machines as enabling technology for all-electric airborne vehicles. Supercond. Sci. Technol. 2007, 20, 748–756. [CrossRef] 19. Brown, G.V. Weights and efficiencies of electric components of a turboelectric aircraft propulsion system. In Proceedings of the 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Orlando, FL, USA, 4–7 January 2011. 20. Kuhn, H.; Seitz, A.; Lorenz, L.; Isikveren, A.T.; Sizmann, A. Progress and perspectives of electric air transport. In Proceedings of the 28th International Congress of the Aeronautical Sciences (ICAS), Brisbane, Australia, 23–28 September 2012. 21. ART First Generation. Available online: http://www.atraircraft.com/products_app/media/pdf/ATR_42- 300-320.pdf (accessed on 31 October 2018). 22. Specific Range Solutions Ltd. Parametric Specific Fuel Consumption Analysis of the PW120A Turboprop Engine. Available online: http://www.srs.aero/wordpress/wp-content/uploads/2009/03/srs-tsd-002-rev- 1-pw120a-sfc-analysis.pdf (accessed on 31 October 2018).PDF Image | Turboprop Hybrid Electric Propulsion System
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