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

There are no files associated with this item.

title単段再使用ロケットにおけるボディフラップ効果のCFD解析
Other TitleCFD analysis of an aerodynamic body-flap effect for a basic SSTO-rocket configuration
Author(jpn)藤本 圭一郎; 藤井 孝蔵
Author(eng)Fujimoto, Keiichiro; Fujii, Kozo
Author Affiliation(jpn)東京大学 大学院; 宇宙航空研究開発機構 宇宙科学研究本部
Author Affiliation(eng)University of Tokyo Graduate School; Japan Aerospace Exploration Agency Institute of Space and Astronautical Science
Issue Date2004-05
PublisherInstitute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)
宇宙航空研究開発機構宇宙科学研究本部
Publication title宇宙航行の力学シンポジウム 平成15年度
Symposium on Flight Mechanics and Astrodynamics 2003
Start page63
End page66
Publication date2004-05
Languagejpn
AbstractNavier-Stokes simulations are carried out for the investigation of a body-flap effect on the subsonic to supersonic base-entry aerodynamic characteristics for the conical SSTO-rocket configuration. It is clarified that the body-flap effect has strong dependence on the angle of attack and Mach number. The body-flap effect is small at subsonic and transonic conditions. At the subsonic and transonic conditions, the windside pressure level over the body-flap is not so high as compared to the leeside due to the influence of the flow which is accelerated over the base surface. It is also clarified that the pressure level behind the body-flap does not become lower than that in the recirculating flow behind the body in all the subsonic to supersonic conditions.
Keywordsreusable rocket; SSTO-rocket; body-flap effect; CFD; angle of attack; Mach number; aerodynamic characteristic; Baldwin-Lomax turbulence model; 再使用型ロケット; SSTOロケット; ボディフラップ効果; CFD; 迎角; マッハ数; 空力特性; Baldwin-Lomax乱流モデル
Document TypeConference Paper
JAXA Categoryシンポジウム・研究会
SHI-NOAA0047120017
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/56400


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