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Evaluation of Dual-Mode Combustor Characteristics with Vitiated and non-Vitiated Inflow
https://jaxa.repo.nii.ac.jp/records/38636
https://jaxa.repo.nii.ac.jp/records/386369f9f79a0-10b5-4fba-9a0d-88e84b0eb618
Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Evaluation of Dual-Mode Combustor Characteristics with Vitiated and non-Vitiated Inflow | |||||
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_5794 | |||||
資源タイプ | conference paper | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
著者 |
Noda, Junji
× Noda, Junji× 富岡, 定毅× 櫻中, 登× 平岩, 徹夫× Noda, Junji× Tomioka, Sadatake× Sakuranaka, Noboru× Hiraiwa, Tetsuo |
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著者所属 | ||||||
東北大学 | ||||||
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(英) | ||||||
en | ||||||
Tohoku University | ||||||
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) | ||||||
出版者(英) | ||||||
出版者 | American Institute of Aeronautics and Astronautics(AIAA) | |||||
書誌情報 | 発行日 2013-07 | |||||
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 | Joint Propulsion Conferences, 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference(July 14-17, 2013.), San Jose, California, United States. | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Supersonic combustion tests were conducted with a direct connected dual-mode combustor. To generate high enthalpy flow, either a hydrogen fueled vitiation heater or a storage heater was used to compare the inflow vitiation effects on the combustor wall pressure distributions. Regarding the storage heated flow, two stagnation temperature conditions were tested. One had a same level stagnation temperature to the vitiated flow, and the other was a higher stagnation temperature which was estimated to gives a matching pressure increase between vitiated and clean air flow. The experimental results showed that the pressure increase ratio of this higher stagnation temperature condition with clean flow seemed to give slightly smaller pressure magnitudes compared to the vitiated flow case at same equivalence ratio. In addition, OH radical gave small effects on pressure distributions. | |||||
DOI | ||||||
識別子タイプ | DOI | |||||
関連識別子 | http://dx.doi.org/10.2514/6.2013-3746 | |||||
関連名称 | info:doi/10.2514/6.2013-3746 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AC1400061000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: AIAA2013-3746 |