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微小重力環境を利用した均一分散燃料噴霧の燃焼実験
https://jaxa.repo.nii.ac.jp/records/13070
https://jaxa.repo.nii.ac.jp/records/130703f3fe9ac-e64e-4e92-822c-09be10414feb
名前 / ファイル | ライセンス | アクション |
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65129010.pdf (369.6 kB)
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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 | ||||||
タイトル | 微小重力環境を利用した均一分散燃料噴霧の燃焼実験 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Spray Combustion | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Uniform Spray | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Flame | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Burner | |||||
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 | Combustion experiments on mono-dispersed fuel spray using microgravity conditions | |||||
著者 |
野村, 浩司
× 野村, 浩司× 相原, 秀紀× 菊池, 政雄× Nomura, Hiroshi× Aihara, Hideki× Kikuchi, Masao |
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著者所属 | ||||||
日本大学 | ||||||
著者所属 | ||||||
日本大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Nihon University | ||||||
著者所属(英) | ||||||
en | ||||||
Nihon University | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS) | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | |||||
書誌情報 |
宇宙利用シンポジウム: 第27回: 平成22年度 en : Space Utilization Research, Vol. 27 2011: Proceedings of The Twenty-seventh Space Utilization Symposium 巻 27, p. 23-24, 発行日 2011-03 |
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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27回宇宙利用シンポジウム (2011年1月24日-25日, 宇宙航空研究開発機構宇宙科学研究所相模原キャンパス), 相模原市, 神奈川県 | |||||
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 | The Twenty-seventh Space Utilization Symposium (January 24-25, 2011. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Mono-dispersed fuel spray with narrow droplet diameter distribution (uniform spray) has been studied with several experimental apparatuses for microgravity. Spherical flame propagation was observed with the constant-pressure chamber and constant-volume chamber, and flame propagation speed and maximum burning pressure were measured with varying mean droplet diameter, total equivalence ratio, liquid equivalence ratio, gas equivalence ratio and pressure. Detailed observations of a flame stabilized in a uniform spray stream were performed with the uniform spray burners. The size of the uniform spray burner has been reduced to fit the combustion experimental module for ISS. | |||||
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 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10324210 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0065129010 |