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HOPEの極超音速流数値シミュレーション検証と応用
https://jaxa.repo.nii.ac.jp/records/43436
https://jaxa.repo.nii.ac.jp/records/434364ff4bd84-8ac5-467c-934b-b06ea3e024f8
名前 / ファイル | ライセンス | アクション |
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nalsp0014003.pdf (1.3 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | HOPEの極超音速流数値シミュレーション検証と応用 | |||||
言語 | ||||||
言語 | jpn | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Numerical Simulation of Hypersonic Flow Around H-II Orbiting Plane | |||||
著者 |
山本, 行光
× 山本, 行光× 秋元, 敏男× 鈴木, 尚行× Yamamoto, Yukimitsu× Akimoto, Toshio× Suzuki, Naoyuki |
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著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
宇宙開発事業団 | ||||||
著者所属 | ||||||
AES Inc | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Space Development Agency of Japan | ||||||
著者所属(英) | ||||||
en | ||||||
AES Inc | ||||||
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 en : Special Publication of National Aerospace Laboratory SP-14 巻 14, p. 19-26, 発行日 1990-11 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | An unmanned winged vehicle for space transportation called H-II Orbiting Plane (HOPE) are being studied by National Space Development Agency of JAPAN (NASDA). In the present paper, hypersonic computational fluid dynamics (CFD) analyses have been performed for HOPE 63 model proposed by NASDA. The effects of Reynolds Number, Mach number, angles of attack, and yaw angles are investigated in detail. In order to use CFD for more practical designing purposes, analyses of control surfaces and gas jet are also made. In addition, calculations of chemically nonequilibrium hypersonic flow are conducted for OREX (Orbiter Re-entry Experiment) model. The purposes of the present study are 1) to demonstrate the validity of the numerical code for aerothemodynamic heating, 2) to investigate the applicability of CFD for control problems, and 3) to develop reliable real gas CFD code. Numerical simulations have been done by using flux-split upwind Navier-Stokes cede. | |||||
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: NALSP0014003 | |||||
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-14 |