文献
J-GLOBAL ID:201902241238697368
整理番号:19A0518018
ガスタービンエンジンの過渡状態における最適制御設計のための新しい方法【JST・京大機械翻訳】
A New Method for the Design of Optimal Control in the Transient State of a Gas Turbine Engine
著者 (4件):
Yu Bing
(Jiangsu Province Key Laboratory of Aerospace Power Systems, College of energy and power engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China)
,
Cao Can
(Jiangsu Province Key Laboratory of Aerospace Power Systems, College of energy and power engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China)
,
Shu Wenjun
(Jiangsu Province Key Laboratory of Aerospace Power Systems, College of energy and power engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China)
,
Hu Zhongzhi
(Jiangsu Province Key Laboratory of Aerospace Power Systems, College of energy and power engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China)
資料名:
IEEE Access
(IEEE Access)
巻:
5
ページ:
23848-23857
発行年:
2017年
JST資料番号:
W2422A
ISSN:
2169-3536
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)