書誌事項
- タイトル別名
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- Aerodynamic Analysis of Membrane Wing Airfoil at Low Reynolds Numbers
抄録
<p>Mars aircraft has been proposed as a means of extensive Mars exploration. Recent research reveals that membrane wings are effective in obtaining sufficient lift in a compact size. In this study, the aerodynamic analysis was performed by forced vibrating the wing under low Reynolds number conditions. As a result, it was found that the flows around the wing and wakes were highly affected by the geometry change.</p>
収録刊行物
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- 計算力学講演会講演論文集
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計算力学講演会講演論文集 2022.35 (0), 23-05-, 2022
一般社団法人 日本機械学会
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キーワード
詳細情報 詳細情報について
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- CRID
- 1390859160311362176
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- ISSN
- 24242799
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- 本文言語コード
- ja
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- データソース種別
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- JaLC
- Crossref
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- 抄録ライセンスフラグ
- 使用不可