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LS-FLOW によるエチレン燃料スクラムジェット燃焼器流れの解析: 燃焼ガス組成の比較
https://jaxa.repo.nii.ac.jp/records/2947
https://jaxa.repo.nii.ac.jp/records/29477b7601e9-6901-46ac-b909-da2b38bf0f2f
名前 / ファイル | ライセンス | アクション |
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2019-02-28 | |||||
タイトル | ||||||
タイトル | LS-FLOW によるエチレン燃料スクラムジェット燃焼器流れの解析: 燃焼ガス組成の比較 | |||||
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 | Numerical Simulation of Ethylene-fueled Scramjet Combustor Flow by Using LS-FLOW Solver: Comparison of the Combustion Gas Composition | |||||
著者 |
高橋, 政浩
× 高橋, 政浩× 野島, 清志× 清水, 太郎× 青野, 淳也× 宗像, 利彦× Takahashi, Masahiro× Nojima, Kiyoshi× Shimizu, Taro× Aono, Junya× Munakata, Toshihiko |
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著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
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 | ||||||
株式会社計算力学研究センター | ||||||
著者所属 | ||||||
株式会社日立ソリューションズ東日本 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (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 | ||||||
Research Center of Computational Mechanics, Inc. | ||||||
著者所属(英) | ||||||
en | ||||||
Hitachi Solutions East Japan, Ltd. | ||||||
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50回流体力学講演会/第36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 50th Fluid Dynamics Conference / the 36th Aerospace Numerical Simulation Symposium 巻 JAXA-SP-18-005, p. 159-164, 発行日 2019-02-25 |
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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50回流体力学講演会/第36回航空宇宙数値シミュレーション技術シンポジウム (2018年7月4日-6日. 宮崎市民プラザ), 宮崎市, 宮崎 | |||||
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 | 50th Fluid Dynamics Conference /the 36th Aerospace Numerical Simulation Symposium (July 4-6, 2018. Miyazaki Citizen's Plaza), Miyazaki, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | RANS simulation corresponding to combustion tests of an ethylene-fueled scramjet combustor model was conducted by using a JAXA in-house solver LS-FLOW. For evaluation of the validity of the present CFD, the profiles of the combustion gas composition on the combustor exit plane predicted by the CFD were compared with experimental ones measured by using a gas sampling rake probe. Good agreement between the CFD and the gas sampling results was obtained at the center plane in the span-wise direction, but agreement was not good for the profiles at the other planes. Influence of both the turbulent Schmidt number and the C2H4-Air combustion mechanism used for the CFD on the numerical results were also examined. The turbulent Schmidt number showed strong influence on the numerical results and the small value of 0.3 resulted in better agreement with the experimental results than 0.89 in the present case. It was also shown that the difference of the combustion mechanisms did not show significant influence on the CFD results in the present case. | |||||
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 | |||||
ISSNONLINE | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 2433-2232 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA1830029018 | |||||
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-18-005 |