Aerodynamic Analysis of Membrane Wing Airfoil at Low Reynolds Numbers

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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

Abstract

<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>

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