文献
J-GLOBAL ID:202002262878103549
整理番号:20A0424426
CARDCにおける2.4M×2.4m遷音速風洞用パラシュートの支持機構設計【JST・京大機械翻訳】
Supporting mechanism design of parachutes for 2.4m×2.4m transonic wind tunnel in CARDC
著者 (5件):
Hao Dong
(High Speed Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang, 621000, People’s Republic of China)
,
Zhang Lin
(High Speed Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang, 621000, People’s Republic of China)
,
Yu Jing
(Computational Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang, 621000, People’s Republic of China)
,
Mao Daiyong
(High Speed Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang, 621000, People’s Republic of China)
,
Yang Xianwen
(High Speed Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang, 621000, People’s Republic of China)
資料名:
IOP Conference Series: Materials Science and Engineering
(IOP Conference Series: Materials Science and Engineering)
巻:
715
号:
1
ページ:
012076 (3pp)
発行年:
2020年
JST資料番号:
W5559A
ISSN:
1757-8981
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)