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極超音速ソニックブームの圧力波形輸送に関する研究
https://jaxa.repo.nii.ac.jp/records/4911
https://jaxa.repo.nii.ac.jp/records/4911b6f66c29-7b50-4a95-9f74-b3bf2b7cd80d
名前 / ファイル | ライセンス | アクション |
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64672013.pdf (738.1 kB)
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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 | 極超音速ソニックブームの圧力波形輸送に関する研究 | |||||
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_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 | Study on Sonic-Boom Propagation of Hypersonic Vehicle | |||||
著者 |
深川, 寛也
× 深川, 寛也× 上野, 篤史× 綿貫, 忠晴× 今村, 宰× 鈴木, 宏二郎× Fukagawa, Tomoya× Ueno, Atsushi× Watanuki, Tadaharu× Imamura, Osamu× Suzuki, Kojiro |
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著者所属 | ||||||
東京大学大学院 | ||||||
著者所属 | ||||||
東京大学大学院新領域創成科学研究科 | ||||||
著者所属 | ||||||
東京大学大学院工学系研究科 | ||||||
著者所属 | ||||||
東京大学大学院工学系研究科 | ||||||
著者所属 | ||||||
東京大学大学院新領域創成科学研究科 | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Advanced Energy, Graduate School of Frontier Science, University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Advanced Energy, Graduate School of Frontier Science, University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
School of Engineering, The University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
School of Engineering, The University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Advanced Energy, Graduate School of Frontier Science, University of Tokyo | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料: 第41回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2009論文集 en : JAXA Special Publication: Proceedings fo 41st Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2009 巻 JAXA-SP-09-011, 発行日 2010-02-26 |
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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 | 平成21年6月18-19日. 宇宙航空研究開発機構調布航空宇宙センター | |||||
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 | 18 June-19 June, 2009, Japan Aerospace Exploration Agency | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Inviscid numerical analysis using the Space-Marching Method was conducted to simulate the sonic-boom propagation, emitted from an axisymmetric palaboric object at Mach 2 and 5. A near-field waveform at four times the body length from the body axis (h/l=4) was calculated using Time-Marching Method. Using Space-Marching Method, the near-field waveform was extrapolated to the mid-field (h/l = from 8 to 30). Comparison with the results obtained from using only time-marching method shows that the present Space-Marching Method is an accurate, high resolving and time-efficient method for predicting sonic-boom propagation. Comparison with the linear supersonic theory clarifies that the sonic-boom prediction by the linear theory becomes inconsistent with numerical results in hypersonic flows. Near-field pressure distributions of an axisymmetric palaboric object at Mach 7 were obtained from the hypersonic wind tunnel experiments, and compared with the numerical results. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0064672013 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-09-011 |