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J-GLOBAL ID:201902232158874953   Reference number:19A2830055

Fuel Burn of an Aircraft with Lightweight ICR Engines Using Airfoil Heat Exchangers

翼型熱交換器で構築した軽量ICRエンジン搭載航空機のフューエルバーン
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Volume: 47  Issue:Page: 429-436  Publication year: Nov. 20, 2019 
JST Material Number: X0134A  ISSN: 0387-4168  Document type: Article
Article type: 原著論文  Country of issue: Japan (JPN)  Language: JAPANESE (JA)
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Gas turbines 
Reference (15):
  • Japan Aircraft Development Corporation, JADC Worldwide Market Forcast 2018-2037, Tokyo Japan, 2018.
  • THE ADVISORY COUNCIL FOR AERONAUTICS RESEARCH IN EUROPE (ACARE), Aeronautics and air transport: beyond vision 2020 (towards 2050) : background document, 2010.
  • Nomura, T., Takahashi, N., Hisa, S., Miyahara, A., and Takakura, M., ′′Fundamental Feasibility Study of Fuel Cell Aircraft′′ 47th Aircraft Symposiun, JSASS-2009-5043, pp.235-240, 2009.
  • Andrew, R., Vishal, S., Florian, J., Joshua, S., ′′Scale Effects on Conventional and Intercooled Turbofan Engine Performance′′, ISABE-2017-22659, 2017.
  • Rolt, A.M. and Baker, N.J., Intercooled turbofan engine design and technology research in the EU Framework 6 NEW AC Programme, 18th International Symposium on Air Breathing Engines ISABE 2009, ISABE-2005-1156, 2005.
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