文献
J-GLOBAL ID:201902243749267112
整理番号:19A2350051
ターボ過給機による航空機燃料タンク慣性システムの性能解析【JST・京大機械翻訳】
Performance analysis of aircraft fuel tank inerting system with turbocharger
著者 (5件):
Li Chaoyue
(Key Laboratory of Aircraft Environment Control and Life Support of MIIT, College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China)
,
Feng Shiyu
(Key Laboratory of Aircraft Environment Control and Life Support of MIIT, College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China)
,
Chen Chen
(Key Laboratory of Aircraft Environment Control and Life Support of MIIT, College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China)
,
Peng Xiaotian
(Key Laboratory of Aircraft Environment Control and Life Support of MIIT, College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China)
,
Liu Weihua
(Key Laboratory of Aircraft Environment Control and Life Support of MIIT, College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China)
資料名:
Proceedings of the Institution of Mechanical Engineers. Part G. Journal of Aerospace Engineering
(Proceedings of the Institution of Mechanical Engineers. Part G. Journal of Aerospace Engineering)
巻:
233
号:
14
ページ:
5217-5226
発行年:
2019年
JST資料番号:
T0823A
ISSN:
0954-4100
資料種別:
逐次刊行物 (A)
記事区分:
原著論文
発行国:
アメリカ合衆国 (USA)
言語:
英語 (EN)