WEKO3
インデックスリンク
アイテム
Stabilization Time of Wake Behind Hypersonic Capsule
https://fukuyama-u.repo.nii.ac.jp/records/8120
https://fukuyama-u.repo.nii.ac.jp/records/8120c61edb5a-e6c0-4d40-9d89-3c1afeb2dae0
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
KJ00005781505.pdf (7.3 MB)
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| Item type | 紀要論文(ELS) / Departmental Bulletin Paper(1) | |||||
|---|---|---|---|---|---|---|
| 公開日 | 2002-12-01 | |||||
| タイトル | ||||||
| タイトル | Stabilization Time of Wake Behind Hypersonic Capsule | |||||
| 言語 | en | |||||
| 言語 | ||||||
| 言語 | eng | |||||
| キーワード | ||||||
| 言語 | en | |||||
| 主題Scheme | Other | |||||
| 主題 | Stabilization time | |||||
| キーワード | ||||||
| 言語 | en | |||||
| 主題Scheme | Other | |||||
| 主題 | Wake | |||||
| キーワード | ||||||
| 言語 | en | |||||
| 主題Scheme | Other | |||||
| 主題 | Hypersonic vehicle | |||||
| キーワード | ||||||
| 言語 | en | |||||
| 主題Scheme | Other | |||||
| 主題 | Electrical discharge method | |||||
| 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 | departmental bulletin paper | |||||
| ページ属性 | ||||||
| 内容記述タイプ | Other | |||||
| 内容記述 | P(論文) | |||||
| 論文名よみ | ||||||
| その他のタイトル | Stabilization Time of Wake Behind Hypersonic Capsule | |||||
| 著者名よみ | ||||||
| 識別子Scheme | WEKO | |||||
| 識別子 | 43552 | |||||
| 姓名 | セザキ, シンジ | |||||
| 著者名よみ | ||||||
| 識別子Scheme | WEKO | |||||
| 識別子 | 43553 | |||||
| 姓名 | ナカムラ, ヒロアキ | |||||
| 著者名よみ | ||||||
| 識別子Scheme | WEKO | |||||
| 識別子 | 43554 | |||||
| 姓名 | ニシオ, マサトミ | |||||
| 著者名(英) | ||||||
| 識別子Scheme | WEKO | |||||
| 識別子 | 43555 | |||||
| 姓名 | SEZAKI, Shinji | |||||
| 言語 | en | |||||
| 著者名(英) | ||||||
| 識別子Scheme | WEKO | |||||
| 識別子 | 43556 | |||||
| 姓名 | NAKAMURA, Hiroaki | |||||
| 言語 | en | |||||
| 著者名(英) | ||||||
| 識別子Scheme | WEKO | |||||
| 識別子 | 43557 | |||||
| 姓名 | NISHIO, Masatomi | |||||
| 言語 | en | |||||
| 著者所属(日) | ||||||
| 値 | 福山大学工学部機械工学科 | |||||
| 著者所属(日) | ||||||
| 値 | 福山大学工学部機械工学科 | |||||
| 著者所属(日) | ||||||
| 値 | 福山大学工学部機械工学科 | |||||
| 著者所属(英) | ||||||
| 言語 | en | |||||
| 値 | Department of Mechanical Engineering, Faculty of Engineering, Fukuyama University | |||||
| 著者所属(英) | ||||||
| 言語 | en | |||||
| 値 | Department of Mechanical Engineering, Faculty of Engineering, Fukuyama University | |||||
| 著者所属(英) | ||||||
| 言語 | en | |||||
| 値 | Department of Mechanical Engineering, Faculty of Engineering, Fukuyama University | |||||
| 抄録(英) | ||||||
| 内容記述タイプ | Other | |||||
| 内容記述 | A stabilization time of a wake structure behind a hypersonic vehicle is very important in an experiment on the flow structure by using pulsed facilities of high enthalpy or of high Mach number. However, observations themselves of such wake structure have been very difficult, and therefore, the experimental discussion about the stabilization time itself has also been very difficult. In this study the stabilization time of the wake structure was formulated by using the dimensional analysis and the present experimental results. The experiment was carried out by observing separation points and free shear layers just after capsule models similar to a MESUR pathfinder probe. To visualize the wake structure, one of techniques called the electrical discharge method was utilized. From these investigations it was found that the stabilization time of the wake structure was related to the Reynolds number, the model scale, and the freestream velocity. A hypersonic gun tunnel of Mach 10 was used in this experiment. | |||||
| 雑誌書誌ID | ||||||
| 収録物識別子タイプ | NCID | |||||
| 収録物識別子 | AN00217655 | |||||
| 書誌情報 |
福山大学工学部紀要 巻 26, p. 179-187, 発行日 2002-12 |
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