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開放端から放出された衝撃波に関する実験と数値シミュレーション(流体工学,流体機械)
https://sucra.repo.nii.ac.jp/records/12646
https://sucra.repo.nii.ac.jp/records/12646093505ab-780e-42c6-afc8-aaf30a8b3935
名前 / ファイル | ライセンス | アクション |
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A3000055.pdf (953.2 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 | 開放端から放出された衝撃波に関する実験と数値シミュレーション(流体工学,流体機械) | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Shock Wave | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Detonation Wave | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Compressible Flow | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Flow Visualization | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Diffraction | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Reflection | |||||
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 | Experiments and Numerical Simulation of a Shock Wave discharged from an Open-end | |||||
著者 |
小原, 哲郎
× 小原, 哲郎× 大八木, 重治× 加藤, 肇× 有賀, 洋介 |
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著者 ローマ字 | ||||||
OBARA, Tetsuro | ||||||
著者 ローマ字 | ||||||
OHYAGI, Shigeharu | ||||||
著者 ローマ字 | ||||||
KATOH, Hajime | ||||||
著者 ローマ字 | ||||||
ARIGA, Yousuke | ||||||
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 68, 号 668, p. 1036-1043, 発行日 2002 |
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年月次 | ||||||
2002-04 | ||||||
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 | It is important to investigate a pressure profile when a diffracted shock wave interacts with a reflector from a safety point of view. Because the diffracted shock waves are often generated by the explosions of combustible gases to cause serious damages against human race and surrounding buildings. The maximum pressure behind reflected shock wave is one of the most important parameter and this report is concerned with the evaluation of maximum pressure, which might be a function of Mach number of the shock wave, distance from a source of the shock wave, initial pressure of the gas, and initial diameter of the shock wave, etc. In this study, a detonation-driven shock tube of 14 m long and 50 mm diameter is used to generate a strong shock wave of propagating Mach number M_S=3.0〜5.2. The shock wave is diffracted from an open end of the shock tube of 25 mm diameter and reflected from a cylindrical reflector of 50 mm diameter. These phenomena are observed using color-schlieren optical techniques and the pressure histories at the stagnation point of the reflector are simultaneously measured. As a result, (i) The behaviors of the diffracted shock wave and complicate flow-fields behind reflected shock wave are observed. (ii) An empirical equation to calculate the maximum pressure behind reflected shock wave is estimated by the results of experimental and numerical simulation. | |||||
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 | ||||||
A3000055 |