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An investigation on the interaction between a supersonic boundary layer and a shock wave produced by the wedge slope
https://doi.org/10.18999/memfenu.21.2.317
https://doi.org/10.18999/memfenu.21.2.317bfba83f8-3495-4aa7-a009-1f9810e43ce6
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
21-2-07.pdf (894.9 kB)
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| Item type | 紀要論文 / Departmental Bulletin Paper(1) | |||||
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| 公開日 | 2021-02-02 | |||||
| タイトル | ||||||
| タイトル | An investigation on the interaction between a supersonic boundary layer and a shock wave produced by the wedge slope | |||||
| 言語 | en | |||||
| 著者 |
Uchida, Shigeo
× Uchida, Shigeo |
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| アクセス権 | ||||||
| アクセス権 | open access | |||||
| アクセス権URI | http://purl.org/coar/access_right/c_abf2 | |||||
| 抄録 | ||||||
| 内容記述タイプ | Abstract | |||||
| 内容記述 | A supersonic boundary layer is interacted by the pressure rise produced by a wedge slope. This interaction is found to be similar with the shock wave reflection from the boundary layer. In the present paper the line of displacement thickness is calculated by the momentum integral equation and the outer supersonic flow along this line is obtained by the theory of linearized supersonic flow Matching the outer and the inner flows, we can solve the entire flow field. The principle of calculation and some numerical results are presented. | |||||
| 言語 | en | |||||
| 出版者 | ||||||
| 出版者 | Faculty of Engineering, Nagoya University | |||||
| 言語 | en | |||||
| 言語 | ||||||
| 言語 | eng | |||||
| 資源タイプ | ||||||
| 資源 | http://purl.org/coar/resource_type/c_6501 | |||||
| タイプ | departmental bulletin paper | |||||
| 出版タイプ | ||||||
| 出版タイプ | VoR | |||||
| 出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||
| ID登録 | ||||||
| ID登録 | 10.18999/memfenu.21.2.317 | |||||
| ID登録タイプ | JaLC | |||||
| ISSN（print） | ||||||
| 収録物識別子タイプ | PISSN | |||||
| 収録物識別子 | 0027-7657 | |||||
| 書誌情報 |
en : Memoirs of the Faculty of Engineering, Nagoya University 巻 21, 号 2, p. 317-330, 発行日 1970-03-31 |
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| 著者版フラグ | ||||||
| 値 | publisher | |||||
