計算力学講演会講演論文集
Online ISSN : 2424-2799
セッションID: 23-05
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低レイノルズ数流れ中で変動する膜翼の空力解析
*中矢 敦士佐々木 大輔高橋 俊川本 裕樹
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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.

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