Aerodynamic Characteristics of a Delta Wing with Arc Camber for Mars Exploration

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

説明

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

収録刊行物

宇宙航空研究開発機構特別資料 = JAXA Special Publication

宇宙航空研究開発機構特別資料 = JAXA Special Publication JAXA-SP-13-001E 343-351, 2013-11-30

宇宙航空研究開発機構(JAXA)

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詳細情報詳細情報について

CRID: 1050292561233852288

NII論文ID: 120006827910

NII書誌ID: AA11984031

ISSN: 1349113X

Web Site: http://id.nii.ac.jp/1696/00004131/

本文言語コード: en

資料種別: conference paper

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