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スクラムジェットエンジン燃焼室の数値解析
https://jaxa.repo.nii.ac.jp/records/43295
https://jaxa.repo.nii.ac.jp/records/432952fcfa167-f99d-4f7e-b42f-048d26c8fc26
名前 / ファイル | ライセンス | アクション |
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nalsp0009004.pdf (385.2 kB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | スクラムジェットエンジン燃焼室の数値解析 | |||||
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 Simulations of the Flow Field in a SCRAM Jet Engine Combustor | |||||
著者 |
平井, 研一
× 平井, 研一× Hirai, Ken-ichi |
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著者所属 | ||||||
日産自動車株式会社 | ||||||
著者所属(英) | ||||||
en | ||||||
Nissan Motor Co. | ||||||
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-9 巻 9, p. 21-26, 発行日 1988-12 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The flow fields over rearward facing step are investigated numerically for the purpose of qualitative understanding of the fuel injection system in the SCRAM jet engine combustor. The results show that the location of transverse injection in relation to the step has significant influence on the size of recirculation zone. | |||||
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: NALSP0009004 | |||||
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-9 |