JAXA Repository / AIREX 未来へ続く、宙(そら)への英知

There are no files associated with this item.

Other TitleNumerical Simulation of Hypersonic Shock Wave Propagation In A Tube Using a Moving Grid Method
Author(jpn)森山, 康平; 酒井, 武治; 丹野, 英幸
Author(eng)Moriyama, Kohei; Sakai, Takeharu; Tanno, Hideyuki
Author Affiliation(jpn)鳥取大学工学部; 鳥取大学; 宇宙航空研究開発機構(JAXA)
Author Affiliation(eng)Tottori University; Tottori University; Japan Aerospace Exploration Agency (JAXA)
Issue Date2019-03
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)
Publication title平成30年度衝撃波シンポジウム 講演論文集
Proceedings of the Symposium on Shock Waves in Japan, FY2018
Publication date2019-03
Description会議情報: 平成30年度衝撃波シンポジウム (2019年3月5日-7日. 横浜国立大学経済・経営学部講義棟1号館 )横浜市, 神奈川県
Meeting Information: Symposium on Shock Waves in Japan, FY2018 (March 5-7, 2019. Yokohama National University), Yokohama, Kanagawa
KeywordsShock Wave propagation; Moving grid; Laminar boundary layer thickness
Document TypeConference Paper
JAXA Categoryシンポジウム・研究会
Report No2A1-4

Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.