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Shock Wave and Viscous Layer Structure in a Rarefied Hypersonic Flow Near the Leading Edge of a Sharp Flat Plate
https://jaxa.repo.nii.ac.jp/records/34399
https://jaxa.repo.nii.ac.jp/records/34399b1c22ee8-413d-4b88-b61b-478988d77a87
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
SA2400571.pdf (822.8 kB)
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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 | Shock Wave and Viscous Layer Structure in a Rarefied Hypersonic Flow Near the Leading Edge of a Sharp Flat Plate | |||||||
| 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 |
OGUCHI, Hakuro
× OGUCHI, Hakuro
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| 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 32, 号 11, p. 233-250, 発行日 1967-12 |
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| 抄録（英） | ||||||||
| 内容記述タイプ | Other | |||||||
| 内容記述 | In the present paper an analysis is presented for the merged layer regime of a hypersonic flow past a semi-infinite flat plate with a sharp leading edge. The analysis is based on the continuum flow theory. The viscous layer solution which is similar to one previously derived by the author is found to patch with the shock-wave-structure solution. The density ratio across the shock and the ratio of shock thickness to viscous layer thickness are evaluated. The results indicate a consistent agreement with the experimental data which were obtained concerning the flow detail by McCroskey et al and by Becker et al. | |||||||
| 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: SA2400571000 | |||||||
