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首页> 外文期刊>Journal of Fluids Engineering: Transactions of the ASME >On the Flutter and Drag Forces on Flexible Rectangular Canopies in Normal Flow
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On the Flutter and Drag Forces on Flexible Rectangular Canopies in Normal Flow

机译:正常流动中柔性矩形遮篷的颤振和阻力

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The paper presents results of experimental investigations on flexible rectangular canopies fixed at two edges (tapes). Data are presented for the aerodynamic drag as a function of the planform area, the slenderness, and the Reynolds number. The slenderness varies from 3.3 to 30. The Reynolds number is limited to 2 X 10~(6). The wind speed is in the range 6-19 m/s. The results show that the drag decreases with the increasing aspect ratio. The dominant parameter is the slenderness; a second dominant factor is the planform area. The drag is only weakly dependent on the Reynolds number. The analysis of the drag data indicates that a proper scaling parameter is the crosswise length scale. When normalization is done, the data tend to collapse into a single curve. A further study addressed the drag characteristics of the canopies with perforated planforms. Perforation of up to 6percent of the planform area has been considered. Corrections for air permeability of the fabric are introduced. The drag is reduced roughly linearly with perforated area. A detailed study into the flutter characteristics of the canopies in the turbulent wind is presented. The investigation has highlighted different modes of oscillations, including deformations through folding and twisting, vertical flapping, rotations, and cross-type oscillations.
机译:本文介绍了固定在两个边缘(胶带)上的柔性矩形遮篷的实验研究结果。呈现的空气阻力数据是平面面积,细长度和雷诺数的函数。细长度从3.3到30不等。雷诺数限制为2 X 10〜(6)。风速为6-19 m / s。结果表明,阻力随着纵横比的增加而减小。主导参数是细长度。第二个主要因素是平面面积。阻力仅微弱地依赖于雷诺数。阻力数据的分析表明适当的缩放参数是横向长度缩放。完成归一化后,数据倾向于折叠为一条曲线。进一步的研究解决了带有穿孔平面的檐篷的阻力特性。已考虑对平面区域进行多达6%的穿孔。介绍了织物透气性的校正方法。阻力随穿孔面积大致线性减小。提出了对湍流中冠层颤振特性的详细研究。该研究强调了不同的振荡模式,包括折叠和扭曲变形,垂直拍打,旋转和十字型振荡。

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