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Aerodynamic Characteristics of a Delta Wing with Arc Camber for Mars Exploration
https://jaxa.repo.nii.ac.jp/records/4137
https://jaxa.repo.nii.ac.jp/records/4137e5fbc258-cc78-49d9-879e-3eea0b492bb6
名前 / ファイル | ライセンス | アクション |
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62070029.pdf (440.2 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 | ||||||
言語 | en | |||||
タイトル | Aerodynamic Characteristics of a Delta Wing with Arc Camber for Mars Exploration | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Delta wing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Arc camber | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Aerodynamics | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Mars exploration | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Three-component force balance | |||||
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 | |||||
著者 |
鵜ノ口, 孝雄
× 鵜ノ口, 孝雄× 青山, 省吾× 末村, 紘志× 山田, 剛治× 松野, 隆× 大林, 茂× 川添, 博光× Unoguchi, Takao× Aoyama, Shogo× Suemura, Hiroshi× Yamada, Gouji× Matsuno, Takashi× Obayashi, Shigeru× Kawazoe, Hiromitsu |
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著者所属 | ||||||
鳥取大学 | ||||||
著者所属 | ||||||
鳥取大学 | ||||||
著者所属 | ||||||
鳥取大学 | ||||||
著者所属 | ||||||
鳥取大学大学院工学研究科機械宇宙工学専攻 | ||||||
著者所属 | ||||||
鳥取大学大学院工学研究科機械宇宙工学専攻 | ||||||
著者所属 | ||||||
東北大学流体科学研究所 | ||||||
著者所属 | ||||||
鳥取大学大学院工学研究科機械宇宙工学専攻 | ||||||
著者所属(英) | ||||||
en | ||||||
Tottori University | ||||||
著者所属(英) | ||||||
en | ||||||
Tottori University | ||||||
著者所属(英) | ||||||
en | ||||||
Tottori University | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Mechanical and Aerospace Engineering, Graduate School of Engineering, Tottori University | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Mechanical and Aerospace Engineering, Graduate School of Engineering, Tottori University | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Fluid Science, Tohoku University | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Mechanical and Aerospace Engineering, Graduate School of Engineering, Tottori University | ||||||
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 en : JAXA Special Publication 巻 JAXA-SP-13-001E, p. 343-351, 発行日 2013-11-30 |
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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 | 5th Symposium on Integrating CFD and Experiments in Aerodynamics (October 3-5, 2012, Chofu Aerospace Center, Japan Aerospace Exploration Agency (JAXA)), Chofu, Tokyo, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In this research, we propose a delta wing with an arc camber to explore the Mars in flight at low Reynolds number of 1.0×10(exp 4) order. The research focuses on L/D of a cambered delta wing to get a wide cross range for the Mars exploration by computational analysis and aerodynamic force measurements using a newly developed three-component force balance. The CFD results show that L/D of the delta wing with an arc camber is much better than the no-camber delta wing at a low angle of attack. Especially, the wing with the camber rate of 5% gives the best performance. The validation results by the EFD approach supports the CFD analysis. | |||||
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: AA0062070029 | |||||
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-13-001E |