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回折する衝撃波の挙動に関する研究 : 第1報, 衝撃波の回折と反射過程
https://sucra.repo.nii.ac.jp/records/12679
https://sucra.repo.nii.ac.jp/records/126791f7f9e0e-cc1f-44e7-b69d-da7556bcaa61
名前 / ファイル | ライセンス | アクション |
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A3000079.pdf (578.6 kB)
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Item type | 学術雑誌論文 / Journal Article(1) | |||||
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公開日 | 2007-09-10 | |||||
タイトル | ||||||
タイトル | 回折する衝撃波の挙動に関する研究 : 第1報, 衝撃波の回折と反射過程 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Compressible Flow | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Computational Fluid Dynamics | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Shock Wave | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Flow Visualization | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | journal article | |||||
タイトル(別言語) | ||||||
その他のタイトル | A Study on Behavior of Diffracted Shock Wave : 1st Report, Process of Shock Wave Diffraction and Reflection | |||||
著者 |
高藤, 亮一
× 高藤, 亮一× 山中, 昭央× 小原, 哲郎× 蔡, 品× 大八木, 重治 |
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著者 ローマ字 | ||||||
TAKAFUJI, Ryouichi | ||||||
著者 ローマ字 | ||||||
YAMANAKA, Akio | ||||||
著者 ローマ字 | ||||||
OBARA, Tetsuro | ||||||
著者 ローマ字 | ||||||
CAI, Pin | ||||||
著者 ローマ字 | ||||||
OHYAGI, Shigeharu | ||||||
著者 所属 | ||||||
埼玉大学大学院理工学研究科 | ||||||
著者 所属(別言語) | ||||||
Graduate School of Science and Engineering, Saitama University | ||||||
書誌情報 |
日本機械学會論文集. B編 巻 65, 号 639, p. 3602-3607, 発行日 1999 |
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年月次 | ||||||
1999-11 | ||||||
出版者名 | ||||||
出版者 | 社団法人日本機械学会 | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 03875016 | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | As is well known when a shock wave is emitted from an open end of a tube, an expansion wave and a vortex ring are generated behind the shock wave. Furthermore, a contact surface, slip line and these wave interactions may cause considerably complicate flow-fields. In this study, shock waves of Mach number 1.3, 1.6 and 2.2 are produced utilizing diaphragm-less shock tube of 50 mm diameter and c. a. 10 m total length, and the flow-fields are visualized with an aid of schlieren optical techniques. A cylindrical reflector is installed at test section and stagnation pressure behind reflected shock wave is measured with wide frequency response. A numerical analysis is also carried out to investigate these flow-fields using Predictor-Corrector TVD finite difference scheme. As a result, (i) the contour of diffracted shock wave is well coincided between experimental and numerical results, (ii) pressure histories behind reflected shock wave are clarified, (iii) an empirical formula is obtained between Mach number, non-dimensional distance from the open end of the tube and non-dimensional pressure just behind reflected shock wave. | |||||
資源タイプ | ||||||
内容記述タイプ | Other | |||||
内容記述 | text | |||||
フォーマット | ||||||
内容記述タイプ | Other | |||||
内容記述 | application/pdf | |||||
作成日 | ||||||
日付 | 2007-03-05 | |||||
日付タイプ | Created | |||||
アイテムID | ||||||
A3000079 |