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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

極超音速衝撃波干渉流れにおける空力加熱の数値解析

http://hdl.handle.net/2237/13871
http://hdl.handle.net/2237/13871
9ea19d5b-9b94-4c06-9e92-ab3d9dd09ee1
名前 / ファイル ライセンス アクション
jjsass_v56_n653_p269.pdf jjsass_v56_n653_p269.pdf (1.8 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 極超音速衝撃波干渉流れにおける空力加熱の数値解析
言語 ja
その他のタイトル
その他のタイトル Numerical Analysis on Aerodynamic Heating in Hypersonic Shock Interacting Flow
言語 en
著者 北村, 圭一

× 北村, 圭一

WEKO 37972

ja 北村, 圭一

Search repository
KITAMURA, Keiichi

× KITAMURA, Keiichi

WEKO 37973

en KITAMURA, Keiichi

Search repository
中村, 佳朗

× 中村, 佳朗

WEKO 37974

ja 中村, 佳朗

Search repository
NAKAMURA, Yoshiaki

× NAKAMURA, Yoshiaki

WEKO 37975

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 Hypersonic Flow
キーワード
主題Scheme Other
主題 Shock Instability
キーワード
主題Scheme Other
主題 Heat Flux
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 Separaion
抄録
内容記述 It is still challenging to predict surface heat-transfer rate in hypersonic flow computations. In this paper, we first performed numerical experiments by changing numerical flux functions and meshes for a hypersonic flow around a hemisphere. Results show that AUSM+ flux function by Liou (1996) on a carefully refined mesh can lead to a shock stable solution with an accurate aerodynamic heating on the surface. Then, a numerical simulation on a hypersonic flow around two bodies involving a shock/shock interaction and a boundary-layer separation has been conducted by using the same method. Although this is a rather difficult problem with a complicated flowfield, comparisons show good agreement with the corresponding experimental data, including the surface heat-transfer rate profile. Therefore, we can say that we have established a numerical method to accurately predict surface heat-transfer in hypersonic shock interacting flows. Finally, detailed analysis of the computed flowfield has been made.
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. 269-277, 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/2237/13871
識別子タイプ HDL
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