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Conceptual Design Methods Hybrid-Electric Transport Aircraft

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Conceptual Design Methods Hybrid-Electric Transport Aircraft ( conceptual-design-methods-hybrid-electric-transport-aircraft )

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118 [112] [113] [114] [115] [116] [117] [118] [119] [120] [121] [122] [123] [124] Bibliography Shaker Haji. Analytical modeling of PEM fuel cell i-V curve. Renewable Energy, 36: 451–458, 2011. doi:10.1016/j.renene.2010.07.007. J.G. Coffin. A Study of Airplane Ranges And Useful Loads. Technical report, NACA Report No.69, 1920. The Boeing Commercial Airplane Company. Cost Index. Technical report, Boeing Flight Operations Engineering, 1990. Clément Pornet, Sascha Kaiser, and Corin Gologan. Cost-Based Flight Technique Optimization for Hybrid Energy Aircraft. DOI 10.1108/ AEAT-05-2014-0075, Aircraft Engineering and Aerospace Technology Journal, 86(6), 2014. doi:10.1108/ AEAT-05- 2014-0075. Lester Faleiro. Beyond the More Electric Aircraft. Aerospace America, (September 2005):35–40, 2005. A A Abdelhafez and A J Forsyth. A Review of More-Electric Aircraft. In 13th Inter- national Conference on Aerospace Science & Aviation Technology - Paper: ASAT-13- EP-01, Cairo, Egypt, 2009. Larry Chick. Assessment of Solid Oxide Fuel Cell Power System for Greener Commercial Aircraft Introduction, Annual Progress Report,. Technical report, Pacific Northwest National Laboratory (PNNL), Richland, WA 99352, 2011. Lester Faleiro, Jacques Herzog, Bernd Schievelbusch, and Taehun Seung. Integrated Equipment Systems for a More Electric Aircraft - Hydraulics and Pneumatics. In 24th International Congress of the Aeronautical Sciences, ICAS - Paper ICAS 2004-7.4.2, 2004. Roland Slingerland, Sijmen Zandstra, Dieter Scholz, and Kolja Seeckt. Green Freighter Systems. Technical report, 2007. S.C. Jensen, G.D. Jenney, and D. Dawson. Flight test experience with an elec- tromechanical actuator on the F-18 Systems Research Aircraft. In 19th DASC. 19th Digital Avionics Systems Conference, IEEE, pages 1–11, 2000. ISBN 0-7803-6395-7. doi:10.1109/DASC.2000.886914. Norio Takahashi, Taku Kondo, Masayuki Takada, Kazuhiro Masutani, Shingo Okano, Mitsuhiro Tsujita, Aerospace Sumitomo, and Precision Products. Development of Pro- totype Electro-Hydrostatic Actuator for Landing Gear Extension and Retraction Sys- tem. In Proceedings of the 7th JFPS International Symposium on Fluid Power, pages 165–168, Toyama, 2008. O Meier and D Scholz. A Handbook Method for the Estimation of Power Requirements for Electrical De-Icing Systems. In DLRK, Hamburg, 2010. DLRK. Xiuxian Xia. Dynamic Power Distribution Management for All Electric Aircraft. PhD thesis, Cranfield University, 2011.

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