Art

J-GLOBAL ID：202002222384418777   Reference number：20A2198703

Classification of supersonic flow over a rigid parachute model with suspension lines

懸垂線を有する剛体パラシュートモデル上の超音速流の分類【JST・京大機械翻訳】

Author (5)： Dahal Nimesh (Graduate School of Integrated Science and Technology, Shizuoka University, Hamamatsu 432-8561, Japan) ,  Fukiba Katsuyoshi (Graduate School of Integrated Science and Technology, Shizuoka University, Hamamatsu 432-8561, Japan) ,  Ito Yusuke (Graduate School of Integrated Science and Technology, Shizuoka University, Hamamatsu 432-8561, Japan) ,  Mizuta Kazuki (Graduate School of Integrated Science and Technology, Shizuoka University, Hamamatsu 432-8561, Japan) ,  Maru Yusuke (Institute of Space and Aeronautical Science, Japan Aerospace Exploration Agency, Sagamihara 252-0222, Japan)
Material： Aerospace Science and Technology  (Aerosp Sci Technol)
Volume： 105  Page： Null  Publication year： 2020 
JST Material Number： W1580A  ISSN： 1270-9638  Document type： Article
Article type： 原著論文  Country of issue： Netherlands (NLD)  Language： ENGLISH (EN)

Abstract/Point： The supersonic wind tunnel tes...

Register(free) or Log In to access     To see more with JDream III (charged).   {{ this.onShowAbsJLink("http://jdream3.com/lp/jglobal/index.html?docNo=20A2198703&from=J-GLOBAL&jstjournalNo=W1580A") }}

Thesaurus term： suspension (disperse system) ,  rigid body ,  shock wave ,  *supersonic flow ,  adhesion (surface chemistry) ,  low pressure ,  supersonic wind tunnel ,  *parachute ,  trailing edge ,  Mach number ,  pressure fluctuation ,  riser ,  catenary ,  canopy ,  mode transition

Author keywords (4)： Supersonic flow ,  Parachute ,  Shock wave ,  Pressure fluctuation

JST classification (2)： Flying object design and structure  (QK04010H) ,  Flight control systems  (QK05020Z)

Terms in the title (6)： 懸垂線 ,  剛体 ,  パラシュート ,  モデル ,  超音速流 ,  分類