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A Comparative Investigation into Aerodynamic Performances of Two Set Finned Bodies with Circular and Non Circular Cross Sections

机译:两套圆形和非圆形截面翅片的空气动力学性能比较研究

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摘要

According to the advantages of noncircular bodies in storage and carriage purposes, these bodies have gained substantial attention by many researchers. In this paper, two circular and square (with rounded corners) bodies, which are attached to two fins, are studied in the free stream Mach number of 0.8.3. The cross section areas of bodies are the same. This work is done using experiment and CFD methods. In the CFD work, a three-dimensional, compressible, stationary, viscous, turbulent flow is simulated using FLUENT code with the standard k-ε model and adaptive grids. The comparison of the results of experiment and CFD simulation shows that the results of CFD are enough accurate. The experiment data in different angles of attack indicate that the square fin-body configuration has higher aerodynamic lift and drag coefficients than the circular one. Also, the results indicate the same aerodynamic performance for both bodies. The results of CFD confirm the deduction obtained from experiment and also they explain the aerodynamic parameters of different parts of fin-body configurations (body alones, bases of bodies, and fins) which are very considerable. The physics of flow is also studied using the pressure contours and velocity vectors.
机译:根据非圆形物体在存储和运输方面的优势,这些物体已受到许多研究人员的广泛关注。在本文中,以0.8.3的自由流马赫数研究了连接到两个散热片的两个圆形和正方形(带有圆角)的物体。主体的横截面积相同。这项工作是使用实验和CFD方法完成的。在CFD工作中,使用带有标准k-ε模型和自适应网格的FLUENT代码来模拟三维可压缩,固定,粘性,湍流。实验结果与CFD仿真结果的比较表明CFD结果足够准确。不同攻角的实验数据表明,方形翅片体结构比圆形翅片体具有更高的空气动力学升力和阻力系数。同样,结果表明两个车身的空气动力学性能相同。 CFD的结果证实了从实验中得出的推论,也解释了翅片-身体构型不同部分(单独的身体,身体的底部和鳍片)的空气动力学参数非常重要。还使用压力轮廓和速度矢量研究了流动的物理性质。

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