文献
J-GLOBAL ID:202202275207150375
整理番号:22A1094436
高揚力低圧タービン翼の境界層の挙動における周期的下流ポテンシャル流の実験的および数値的研究【JST・京大機械翻訳】
Experimental and numerical investigation of periodic downstream potential flow on the behavior of boundary layer of high-lift low-pressure turbine blade
著者 (7件):
Sun Shuang
(Department of Aviation Engineering, Civil Aviation University of China, 2898 Jinbei Road, Dongli District, Tianjin 300300, PR China)
,
Sun Shuang
(State Key Laboratory of Aerodynamics, CARDC, No. 6, South Section, Second Ring Road, Mianyang City, Sichuan Province, 621000, PR China)
,
Wu Xingshuang
(Department of Aviation Engineering, Civil Aviation University of China, 2898 Jinbei Road, Dongli District, Tianjin 300300, PR China)
,
Huang Zhen
(Department of Aviation Engineering, Civil Aviation University of China, 2898 Jinbei Road, Dongli District, Tianjin 300300, PR China)
,
Hu Xizhuo
(Department of Aviation Engineering, Civil Aviation University of China, 2898 Jinbei Road, Dongli District, Tianjin 300300, PR China)
,
Zhang Peng
(Department of Aviation Engineering, Civil Aviation University of China, 2898 Jinbei Road, Dongli District, Tianjin 300300, PR China)
,
Kong Qingguo
(Sino-European Institute of Aviation Engineering, Civil Aviation University of China, 2898 Jinbei Road, Dongli District, Tianjin 300300, PR China)
資料名:
Aerospace Science and Technology
(Aerospace Science and Technology)
巻:
123
ページ:
Null
発行年:
2022年
JST資料番号:
W1580A
ISSN:
1270-9638
資料種別:
逐次刊行物 (A)
記事区分:
原著論文
発行国:
オランダ (NLD)
言語:
英語 (EN)