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再突入飛行体まわりの空力加熱のCFD解析と実験
https://jaxa.repo.nii.ac.jp/records/36870
https://jaxa.repo.nii.ac.jp/records/36870b599aef4-c129-4232-89bc-74cb34bfa1dd
名前 / ファイル | ライセンス | アクション |
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nalsp0034011.pdf (1.2 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 再突入飛行体まわりの空力加熱のCFD解析と実験 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値流体力学 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力加熱 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 再突入飛行体 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 極超音速CFD解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 極超音速風洞 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Calspan衝撃波トンネル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高エンタルピートンネル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | OREX | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道再突入実験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | HYFLEX | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 極超音速飛行実験 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CFD | |||||
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 | aerothermodynamic heating | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | reentry vehicle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hypersonic CFD analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hypersonic wind tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Calspans shock tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | high enthalpy shock tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | OREX | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | orbital reentry experiment | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | HYFLEX | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hypersonic flight experiment | |||||
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 | CFD analysis and experiment of aerothermodynamic heating around re-entry vehicle | |||||
著者 |
山本, 行光
× 山本, 行光× Yamamoto, Yukimitsu |
|||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
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 巻 34, p. 55-60, 発行日 1997-01 |
|||||
会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 航空宇宙技術研究所 6-7 JUN. 1996 東京 日本 | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | National Aerospace Laboratory 6-7 JUN. 1996 Tokyo Japan | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | NAL-M10-HWT(極超音速風洞)、ONERA-S4MA-HWT、Calspans衝撃波トンネル、Caltech-T-5高エンタルピー衝撃波トンネルなどを含む極超音速風洞実験と極超音速CFD(数値流体力学)解析との最近の比較を紹介した。また、OREX(軌道再突入実験機)およびHYFLEX(極超音速飛行実験)などの極超音速再突入飛行解析を行った。これらの研究を通し、再突入機体の熱空力加熱特性を詳細に検討した。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Recent comparisons of hypersonic CFD (Computational Fluid Dynamics) analysis with hypersonic wind tunnel experiments, including NAL M10 HWT (Hypersonic Wind Tunnel), ONERA S4MA HWT, Calspan's shock tunnel and Caltech T-5 high enthalpy shock tunnel, are introduced. Also, hypersonic reentry flight analysis, such as OREX (Orbital Reentry Experiment) and HYFLEX (Hypersonic Flight Experiment) are made. Through these studies, aerothermodynamic heating characteristics of reentry vehicle are investigated in detail. | |||||
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: AA0000685011 | |||||
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-34 |