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デュアルベルノズル・サブスケール燃焼試験における作動点遷移予測について
https://jaxa.repo.nii.ac.jp/records/3491
https://jaxa.repo.nii.ac.jp/records/34918e1a0dd3-e40d-41da-946b-dc4c54008812
名前 / ファイル | ライセンス | アクション |
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AA1630031016.pdf (789.7 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2017-01-13 | |||||
タイトル | ||||||
タイトル | デュアルベルノズル・サブスケール燃焼試験における作動点遷移予測について | |||||
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_5794 | |||||
資源タイプ | conference paper | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Prediction of operation mode transition in combustion tests of a sub-scaled dual-bell nozzle model | |||||
著者 |
高橋, 政浩
× 高橋, 政浩× 高橋, 英美× 冨田, 健夫× Genin, Chloe× Schneider, Dirk× Takahashi, Masahiro× Takahashi, Hidemi× Tomita, Takeo× Genin, Chloe× Schneider, Dirk |
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著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
German Aerospace Center (DLR) | ||||||
著者所属 | ||||||
German Aerospace Center (DLR) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
German Aerospace Center (DLR) | ||||||
著者所属(英) | ||||||
en | ||||||
German Aerospace Center (DLR) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構(JAXA) | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料: 第48回流体力学講演会/第34回航空宇宙数値シミュレーション技術シンポジウム論文集 en : JAXA Special Publication: Proceedings of the 48th Fluid Dynamics Conference / the 34th Aerospace Numerical Simulation Symposium 巻 JAXA-SP-16-007, p. 137-140, 発行日 2016-12-27 |
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会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 第48回流体力学講演会/第34回航空宇宙数値シミュレーション技術シンポジウム (2016年7月6日-8日. 金沢歌劇座), 金沢市, 石川 | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 48th Fluid Dynamics Conference /the 34th Aerospace Numerical Simulation Symposium (July 6-8, 2016. The Kanazawa Theatre), Kanazawa, Ishikawa, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | LOX/GCH4 combustion tests of sub-scaled dual-bell nozzle models have been conducted under research collaboration between DLR and JAXA. In this report, RANS simulation corresponding to these experiments was conducted to understand phenomena of the operation mode-transition and to evaluate prediction capability of the mode-transition condition in case with the combusting gas. The results showed that a turbulence model to be used has strong influence on the predicted mode-transition condition and that influence of an oxidizer-fuel mixture ratio on the mode-transition condition was different between CFD and the experiments. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA1630031016 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-16-007 |