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超音速燃焼器内流れの数値解析
https://jaxa.repo.nii.ac.jp/records/43540
https://jaxa.repo.nii.ac.jp/records/4354033382259-7f63-4e94-a1bd-36a3572b3df7
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
nalsp0016044.pdf (856.9 kB)
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| Item type | テクニカルレポート / Technical Report(1) | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|
| 公開日 | 2015-03-26 | |||||||||
| タイトル | ||||||||||
| タイトル | 超音速燃焼器内流れの数値解析 | |||||||||
| 言語 | ||||||||||
| 言語 | jpn | |||||||||
| 資源タイプ | ||||||||||
| 資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||||||
| 資源タイプ | technical report | |||||||||
| その他のタイトル（英） | ||||||||||
| その他のタイトル | Numerical Calculation of Flow Field in Supersonic Combustion Chamber | |||||||||
| 著者 |
西内, 誠
× 西内, 誠
× Nishiuchi, Makoto
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| 著者所属 | ||||||||||
| 三菱重工業株式会社 | ||||||||||
| 著者所属（英） | ||||||||||
| en | ||||||||||
| Mitsubishi Heavy Industries Ltd. | ||||||||||
| 出版者 | ||||||||||
| 出版者 | 航空宇宙技術研究所 | |||||||||
| 出版者（英） | ||||||||||
| 出版者 | National Aerospace Laboratory(NAL) | |||||||||
| 書誌情報 |
航空宇宙技術研究所特別資料 en : Special Publication of National Aerospace Laboratory SP-16 巻 16, p. 277-282, 発行日 1991-12 |
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| 抄録（英） | ||||||||||
| 内容記述タイプ | Other | |||||||||
| 内容記述 | There has been a renewed interest in hypersonic air breathing propulsion during the last decade. This interest is mainly associated with the study of hypersonic flight vehicles and space planes. A major focus of these studies is to develop new concept in propulsion technology. One of the propulsion concepts is based on supersonic combustion ramjet (Scramjet). However, because of the difficulties in experimentally simulating the actual flight environment, the details of the flow phenomena in the scramjet combustor, in particular the physics and fluid mechanism of the supersonic combustion process, are not well understood. Fortunately the recent progress of supercomputers and the advanced numerical algorithms have made it possible to analyze the combustor flow field with turbulence models and finite rate chemical reactions. In the present study, a numerical algorithm for supersonic flow with Hydrogen/Air combustion was developed, and two test cases were computed. These results are compared with existing available computational and experimental results. | |||||||||
| ISSN | ||||||||||
| 収録物識別子タイプ | ISSN | |||||||||
| 収録物識別子 | 0289-260X | |||||||||
| 書誌レコードID | ||||||||||
| 収録物識別子タイプ | NCID | |||||||||
| 収録物識別子 | AN10097345 | |||||||||
| 資料番号 | ||||||||||
| 内容記述タイプ | Other | |||||||||
| 内容記述 | 資料番号: NALSP0016044 | |||||||||
| レポート番号 | ||||||||||
| 内容記述タイプ | Other | |||||||||
| 内容記述 | レポート番号: NAL SP-16 | |||||||||
