@inproceedings{oai:jaxa.repo.nii.ac.jp:00004137,
 author = {鵜ノ口, 孝雄 and 青山, 省吾 and 末村, 紘志 and 山田, 剛治 and 松野, 隆 and 大林, 茂 and 川添, 博光 and Unoguchi, Takao and Aoyama, Shogo and Suemura, Hiroshi and Yamada, Gouji and Matsuno, Takashi and Obayashi, Shigeru and Kawazoe, Hiromitsu},
 book = {宇宙航空研究開発機構特別資料, JAXA Special Publication},
 month = {Nov},
 note = {5th Symposium on Integrating CFD and Experiments in Aerodynamics (October 3-5, 2012, Chofu Aerospace Center, Japan Aerospace Exploration Agency (JAXA)), Chofu, Tokyo, Japan, 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., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0062070029, レポート番号: JAXA-SP-13-001E},
 pages = {343--351},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {Aerodynamic Characteristics of a Delta Wing with Arc Camber for Mars Exploration},
 volume = {JAXA-SP-13-001E},
 year = {2013}
}