WEKO3
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将来型TSTO宇宙輸送システムのための2体問題衝撃波干渉の極超音速風洞検証
https://jaxa.repo.nii.ac.jp/records/38245
https://jaxa.repo.nii.ac.jp/records/382457f966053-8a74-4a0c-b172-d251de67b5eb
名前 / ファイル | ライセンス | アクション |
---|---|---|
nalsp0057024.pdf (2.6 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 | 将来型TSTO宇宙輸送システムのための2体問題衝撃波干渉の極超音速風洞検証 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | TSTO機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衝撃・衝撃相互作用 | |||||
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 | 極超音波風洞 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙輸送 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 仰角 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | シャドーグラフ写真 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衝撃・境界層相互作用 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 研究開発 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 局所ピーク加熱 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衝撃波 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | TSTO vehicle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | shock-shock interaction | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic heating | |||||
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 | space transportation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | angle of attack | |||||
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 | shadowgraph photography | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | shock-boundary layer interaction | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | research and development | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | local peak heating | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | shock wave | |||||
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 | Numerical analysis and hypersonic wind tunnel experiments of complex shock-shock interactions for future TSTO transport problems | |||||
著者 |
山本, 行光
× 山本, 行光× 穂積, 弘一× 戸塚, 亜希子× 金田, 誠× 保阪, 陽子× 上敷領, 早苗× Yamamoto, Yukimitsu× Hozumi, Koichi× Totsuka, Akiko× Kaneda, Makoto× Hosaka, Yoko× Kamishikiryo, Sanae |
|||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
トータルシステム | ||||||
著者所属 | ||||||
三向ソフトウエア開発 | ||||||
著者所属 | ||||||
三向ソフトウエア開発 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
Total System Inc. | ||||||
著者所属(英) | ||||||
en | ||||||
Sanko Software Dept. Co. Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Sanko Software Dept. Co. Ltd. | ||||||
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2002論文集 en : Special Publication of National Aerospace Laboratory: Proceedings of Aerospace Numerical Simulation Symposium 2002 巻 57, p. 136-139, 発行日 2003-03 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Hypersonic aerodynamic heating problem has been investigated for the shock-shock interactions of two hemi-sphere cylinder problem for future TSTO space transport systems. Two hemisphere models with a diameter of 3 cm and 6 cm are placed parallel or with the inclined angles and hypersonic wind tunnel tests have been made by NAL Mach 10 HWT. Severe local peak heating is generated on the small hemisphere nose by strong shock-shock interactions of Type 3 at the inclined angle of 15 deg. In the parallel setting cases at high angles of attack. Type 1 and Type 2 shock interaction patterns are observed. CFD computations can predict local peak heating accurately in the interaction area and the structure of shock-shock, shock-boundary layer interaction can be resolved 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: AA0045948024 | |||||
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-57 |