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  1. B200 工学部/工学研究科
  2. B200a 雑誌掲載論文
  3. 学術雑誌

極超音速TSTOにおける衝撃波干渉・境界層剥離を伴う流れ場の解析

http://hdl.handle.net/2237/13872
http://hdl.handle.net/2237/13872
76aa7d1d-d79d-46bd-9fa2-cd3dcc7879d8
名前 / ファイル ライセンス アクション
jjsass_v56_n653_p278.pdf jjsass_v56_n653_p278.pdf (1.9 MB)
Item type 学術雑誌論文 / Journal Article(1)
公開日 2010-07-27
タイトル
タイトル 極超音速TSTOにおける衝撃波干渉・境界層剥離を伴う流れ場の解析
言語 ja
その他のタイトル
その他のタイトル Investigation on Hypersonic Shock Interacting and Boundary-Layer Separating Flowfield around Two-Stage-To-Orbit Vehicle
言語 en
著者 北村, 圭一

× 北村, 圭一

WEKO 37976

ja 北村, 圭一

Search repository
KITAMURA, Keiichi

× KITAMURA, Keiichi

WEKO 37977

en KITAMURA, Keiichi

Search repository
小澤, 啓伺

× 小澤, 啓伺

WEKO 37978

ja 小澤, 啓伺

Search repository
OZAWA, Hiroshi

× OZAWA, Hiroshi

WEKO 37979

en OZAWA, Hiroshi

Search repository
花井, 勝祥

× 花井, 勝祥

WEKO 37980

ja 花井, 勝祥

Search repository
HANAI, Katsuhisa

× HANAI, Katsuhisa

WEKO 37981

en HANAI, Katsuhisa

Search repository
森, 浩一

× 森, 浩一

WEKO 37982

ja 森, 浩一

Search repository
MORI, Koichi

× MORI, Koichi

WEKO 37983

en MORI, Koichi

Search repository
中村, 佳朗

× 中村, 佳朗

WEKO 37984

ja 中村, 佳朗

Search repository
NAKAMURA, Yoshiaki

× NAKAMURA, Yoshiaki

WEKO 37985

en NAKAMURA, Yoshiaki

Search repository
アクセス権
アクセス権 open access
アクセス権URI http://purl.org/coar/access_right/c_abf2
キーワード
主題Scheme Other
主題 CFD
キーワード
主題Scheme Other
主題 TSTO (Two-Stage-To-Orbit)
キーワード
主題Scheme Other
主題 Hypersonic Flow
キーワード
主題Scheme Other
主題 Shock/Shock Interaction
キーワード
主題Scheme Other
主題 Boundary-Layer Separation
キーワード
主題Scheme Other
主題 UT-Kashiwa Hypersonic and High-Temperature Wind Tunnel
抄録
内容記述 To explore future RLVs, a hypersonic flowfield around a Two-Stage-To-Orbit (TSTO) configuration is analyzed in this paper. This study also demonstrates how CFD, as a powerful tool, can be applied to investigate such a complex flowfield involving a shock/shock interaction and a boundary-layer separation. First, the hypersonic flow around two bodies of the TSTO model has been numerically simulated, and then, the results are validated by comparing with experimental data taken at the UT-Kashiwa Hypersonic Tunnel. Finally, the detailed, computed flowfield is shown to have pairs of streamwise vortices (including horseshoe vortices) with alternating signs of rotation around the TSTO body surfaces.
言語 en
内容記述タイプ Abstract
出版者
言語 ja
出版者 日本航空宇宙学会
言語
言語 jpn
資源タイプ
資源タイプresource http://purl.org/coar/resource_type/c_6501
タイプ journal article
出版タイプ
出版タイプ VoR
出版タイプResource http://purl.org/coar/version/c_970fb48d4fbd8a85
ISSN
収録物識別子タイプ PISSN
収録物識別子 1344-6460
書誌情報 ja : 日本航空宇宙学会論文集

巻 56, 号 653, p. 278-285, 発行日 2008-06-05
フォーマット
application/pdf
著者版フラグ
値 publisher
URI
識別子 http://hdl.handle.net/2237/13872
識別子タイプ HDL
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