Tottori University
Tottori University
Tottori University
Department of Mechanical and Aerospace Engineering, Graduate School of Engineering, Tottori University
Department of Mechanical and Aerospace Engineering, Graduate School of Engineering, Tottori University
Institute of Fluid Science, Tohoku University
Department of Mechanical and Aerospace Engineering, Graduate School of Engineering, Tottori University
出版者
宇宙航空研究開発機構(JAXA)
出版者（英）
Japan Aerospace Exploration Agency (JAXA)
雑誌名
宇宙航空研究開発機構特別資料
雑誌名(英)
JAXA Special Publication
巻
JAXA-SP-13-001E
ページ
343 - 351
発行年
2013-11-30
会議概要（会議名, 開催地, 会期, 主催者等）（英）
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）
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
形態: カラー図版あり
内容記述（英）
Physical characteristics: Original contains color illustrations
Aerodynamic Characteristics of a Delta Wing with Arc Camber for Mars Exploration
62070029.pdf
(440.2KB)
