文献
J-GLOBAL ID:202002214616146808
整理番号:20A0500227
FBOを考慮した融合設計による航空エンジンの応答【JST・京大機械翻訳】
Response of Aeroengine with Fusing Design Suffering FBO
著者 (5件):
Ma Chi
(Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Collaborative Innovation Center of Advanced Aeroengine, Nanjing, Jiangsu Province 210016, China)
,
Chen Wei
(Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Collaborative Innovation Center of Advanced Aeroengine, Nanjing, Jiangsu Province 210016, China)
,
Liu Lulu
(Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Collaborative Innovation Center of Advanced Aeroengine, Nanjing, Jiangsu Province 210016, China)
,
Zhao Zhenhua
(Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Collaborative Innovation Center of Advanced Aeroengine, Nanjing, Jiangsu Province 210016, China)
,
Luo Gang
(Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Collaborative Innovation Center of Advanced Aeroengine, Nanjing, Jiangsu Province 210016, China)
資料名:
International Journal of Aerospace Engineering (Web)
(International Journal of Aerospace Engineering (Web))
巻:
2019
ページ:
Null
発行年:
2019年
JST資料番号:
U7708A
ISSN:
1687-5966
資料種別:
逐次刊行物 (A)
記事区分:
原著論文
発行国:
イギリス (GBR)
言語:
英語 (EN)