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膨張波管内流れにおける境界層の影響に関する数値的研究
https://jaxa.repo.nii.ac.jp/records/4391
https://jaxa.repo.nii.ac.jp/records/43911a55149a-0f47-44f0-867c-43f237cb4568
名前 / ファイル | ライセンス | アクション |
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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 | 膨張波管内流れにおける境界層の影響に関する数値的研究 | |||||
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 | Numerical Study of Boundary Layer Effects in Expansion Tube | |||||
著者 |
赤堀, 敬法
× 赤堀, 敬法× 牧野, 仁× 永田, 靖典× 山田, 和彦× 平岡, 克己× 安部, 隆士× Akahori, Takanori× Makino, Hitoshi× Nagata, Yasunori× Yamada, Kazuhiko× Hiraoka, Katsumi× Abe, Takashi |
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著者所属 | ||||||
東海大学 | ||||||
著者所属 | ||||||
東海大学 | ||||||
著者所属 | ||||||
東京大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS) | ||||||
著者所属 | ||||||
東海大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Tokai University | ||||||
著者所属(英) | ||||||
en | ||||||
Tokai University | ||||||
著者所属(英) | ||||||
en | ||||||
University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Tokai University | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
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43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2011論文集 en : JAXA Special Publication: Proceedings of 43rd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2011 巻 JAXA-SP-11-015, p. 113-118, 発行日 2012-03-30 |
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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 | 第43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2011 (2011年7月7日-8日. 早稲田大学国際会議場) 東京 | |||||
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 | 43rd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2011 (July 7-8, 2011. Waseda University, International Conference Center), Tokyo Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The effect of the boundary layer development associated with the shock wave propagating through the low pressure tube part of the expansion tube was investigated. For this purpose, the low pressure tube flow was simulated by the time-dependent axisymmetric Navier-Stokes equation with ideal gas assumption and coefficient of viscocity of given by Sutherland's formula. It is found that because of the finite formulation process of the shockwave, the initial resultant shock speed exceeds the theoretical prediction but, afterwards, the shock speed keeps decreasing because of the boundary layer development initiated from the intersection of the shock wave and the tube wall. Simultaneously, the contact surface is accelerated. As a result, the region between the shock wave and the contact surface becomes narrow and the test flow arrival becomes faster than the theoretical estimations. The present simulation results agree with the experimental results at least qualitatively. However, numerical calculation models must be improved, such as real gas effects or three dimensional calculation. | |||||
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: AA0065207019 | |||||
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-11-015 |