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Aerodynamic characteristics of airfoils in low Reynolds number

机译:低雷诺数下翼型的空气动力学特性

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摘要

Characteristics of a single airfoil and a turbine cascade in low Reynolds number flows are described based on the results of the wind tunnel experiments. Stall of the single airfoil occurs at low attack angles, and pressure distributions and flow patterns formed by oil flow visualization give the validity. And it is suggested that the similar phenomena likely occur in the turbine cascade also.
机译:根据风洞实验结果,描述了低雷诺数流中单个翼型和涡轮机级联的特性。单个翼型的失速发生在低迎角下,通过油流可视化形成的压力分布和流动模式给出了有效性。并且有人认为,类似的现象也可能发生在涡轮机级联中。

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