文献
J-GLOBAL ID:202102252722903880
整理番号:21A0575991
貫通亀裂を有する一体型航空機翼パネル:応力拡大係数に及ぼす構造パラメータの影響【JST・京大機械翻訳】
Integral Aircraft Wing Panels with Penetration Cracks: The Influence of Structural Parameters on the Stress Intensity Factor
著者 (12件):
Hai Gong
(College of Mechanical and Electrical Engineering, Central South University, Changsha 410083, China)
,
Hai Gong
(Light Alloy Research Institute, Central South University, Changsha 410083, China)
,
Hai Gong
(State Key Laboratory of High Performance Complex Manufacturing, Central South University, Changsha 410083, China)
,
Bin Yi
(College of Mechanical and Electrical Engineering, Central South University, Changsha 410083, China)
,
Bin Yi
(State Key Laboratory of High Performance Complex Manufacturing, Central South University, Changsha 410083, China)
,
Yunxin Wu
(College of Mechanical and Electrical Engineering, Central South University, Changsha 410083, China)
,
Yunxin Wu
(Light Alloy Research Institute, Central South University, Changsha 410083, China)
,
Yunxin Wu
(State Key Laboratory of High Performance Complex Manufacturing, Central South University, Changsha 410083, China)
,
Zhiqi Liao
(College of Mechanical and Electrical Engineering, Central South University, Changsha 410083, China)
,
Zhiqi Liao
(State Key Laboratory of High Performance Complex Manufacturing, Central South University, Changsha 410083, China)
,
Yaoqiong Liu
(Avic The First Aircraft Institute, Xi’an 710000, China)
,
Fei Du
(School of Astronautics, Northwestern Polytechnical University, Xi’an 710072, China)
資料名:
Applied Sciences (Web)
(Applied Sciences (Web))
巻:
10
号:
12
ページ:
4142
発行年:
2020年
JST資料番号:
U7135A
ISSN:
2076-3417
資料種別:
逐次刊行物 (A)
記事区分:
原著論文
発行国:
スイス (CHE)
言語:
英語 (EN)