Abstract:Original scientific paper The deformable membrane airfoils (DMA) are considered in the present paper, which could be potentially used on a new class of modern Micro Aerial Vehicles for their compact and lightweight form. Numerical simulations of low Reynolds number airflow around the DMA with excess length were performed and compared with the results obtained in the experiment. The aerodynamic performance was studied using a fluid-structure interaction between the DMA with excess length and the surrounding flu… Show more
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