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市販コードINCAを用いたHOPE-Xまわりの極超音速流CFD解析
https://jaxa.repo.nii.ac.jp/records/38041
https://jaxa.repo.nii.ac.jp/records/38041ab03c426-f81a-4711-9b23-0bbc7b39745f
名前 / ファイル | ライセンス | アクション |
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nalsp0053005.pdf (1.1 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 市販コードINCAを用いたHOPE-Xまわりの極超音速流CFD解析 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 極超音速流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 計算流体力学 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | HOPE-X | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 再突入 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力特性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞データ | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hypersonic flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | computational fluid dynamics | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numerical analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | HOPE-X | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | reentry | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic characteristic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel data | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Hypersonic CFD analysis of the HOPE-X vehicle by INCA | |||||
著者 |
坂元, 康朗
× 坂元, 康朗× 辻本, 健士× Sakamoto, Yasuro× Tsujimoto, Takeshi |
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著者所属 | ||||||
三菱重工業 | ||||||
著者所属 | ||||||
宇宙開発事業団 | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Heavy Industries Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
National Space Development Agency of Japan | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory (NAL) | |||||
書誌情報 |
航空宇宙技術研究所特別資料: 航空宇宙数値シミュレーション技術シンポジウム2001論文集 en : Special Publication of National Aerospace Laboratory: Proceedings of Aerospace Numerical Simulation Symposium 2001 巻 53, p. 25-28, 発行日 2002-01 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In this paper, some results of hypersonic CFD simulation of HOPE-X vehicle by commercial CFD code 'INCA', which are available for non-equilibrium flow analysis to estimate real gas effect at reentry phase, is presented. Compared with the results by NAL code and wind tunnel, it appears that the commercial CFD solver enables to take some suitable results, so that it is to confirm the tool's potential and the step to define the aerodynamic characteristics in HOPE-X design. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0289-260X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10097345 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0032819005 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL SP-53 |