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An Analysis of Shock Waves in Binary Gas Mixtures with Special Regard to Temperature Overshoot
https://jaxa.repo.nii.ac.jp/records/34489
https://jaxa.repo.nii.ac.jp/records/34489cdb52871-525c-4761-933c-ff4ea8a1b799
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
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| Item type | 紀要論文 / Departmental Bulletin Paper(1) | |||||||||
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| 公開日 | 2015-03-26 | |||||||||
| タイトル | ||||||||||
| タイトル | An Analysis of Shock Waves in Binary Gas Mixtures with Special Regard to Temperature Overshoot | |||||||||
| 言語 | en | |||||||||
| 言語 | ||||||||||
| 言語 | eng | |||||||||
| 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 | |||||||||
| 著者 |
ABE, Kanji
× ABE, Kanji
× OGUCHI, Hakuro
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| 著者所属(英) | ||||||||||
| en | ||||||||||
| Department of Applied Science,Faculty of Engineering,Kyushu University | ||||||||||
| 出版者 | ||||||||||
| 出版者 | 東京大学宇宙航空研究所 | |||||||||
| 出版者(英) | ||||||||||
| 出版者 | Institute of Space and Aeronautical Science,University of Tokyo | |||||||||
| 書誌情報 |
en : ISAS report/Institute of Space and Aeronautical Science,University of Tokyo 巻 39, 号 8, p. 161-172, 発行日 1974-03 |
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| 抄録(英) | ||||||||||
| 内容記述タイプ | Other | |||||||||
| 内容記述 | Shock wave structures in argon-helium mixtures are numerically analysed on the basis of a kinetic model for binary gas mixtures. The results are compared with Harnett and Muntz' experiment, and reasonable agreement between computation and experiment is found. Special attention is paid to the overshoot phenomena of argon temperature. The argon temperature overshoot is shown from the results to occur for a sufficiently small mole fraction of argon. Such overshoot is also shown to occur for a comparatively larger mole fraction of argon, as the shock Mach number becomes higher. | |||||||||
| ISSN | ||||||||||
| 収録物識別子タイプ | ISSN | |||||||||
| 収録物識別子 | 0372-1418 | |||||||||
| 書誌レコードID | ||||||||||
| 収録物識別子タイプ | NCID | |||||||||
| 収録物識別子 | AA00675986 | |||||||||
| 資料番号 | ||||||||||
| 内容記述タイプ | Other | |||||||||
| 内容記述 | 資料番号: SA2400966000 | |||||||||