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Side force over slender body with rings at different location at subsonic speed

机译:细长体上的侧向力以亚音速在不同位置带有环

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摘要

Investigations have been made adopting experiments and computations on an ogive-nosed slender body at different angles of attack and Reynolds number of 29,000 based on the model base diameter diameter. The results indicated an increase in the side force at large angles of attack, which is mainly due to the presence of asymmetric vortices in the leeward of the body. The inclusion of a rectangular cross-sectioned ring in the initial portion of the body reduced the side force at higher angles of attack. However, significant side force was experienced at lower angles of attack (30 degrees40 degrees). Use of a ring of 3% height was found to be suitable for reducing the side force at a higher angle of attack. From the results obtained it was observed that a ring if placed at a different axial location alters the flow field and changes the side force at higher angles of attack. Further studies indicated that placing of rings pair at an axial location of 3.5 and 4.5 times the base diameter reduced the side force to a very low value at all the angles of attack for the present shape of body and flow conditions.
机译:根据模型的基本直径直径,在不同的迎角和29,000雷诺数的情况下,对带有尖齿的细长体进行了实验和计算,进行了研究。结果表明,在大迎角下,侧向力增加了,这主要是由于人体背风处存在不对称涡旋。在主体的初始部分包括一个矩形横截面的环,可以减小较高攻角时的侧向力。但是,在较低的迎角(30度 40度)下会遇到较大的侧向力。发现使用高度为3%的环适合于减小较大攻角下的侧向力。从获得的结果可以观察到,如果环放置在不同的轴向位置,则会改变流场并在较大的迎角下改变侧向力。进一步的研究表明,将环对放置在基本直径的3.5倍和4.5倍的轴向位置上,对于当前的机体形状和流动条件,在所有迎角下,侧向力均会减小至非常低的值。

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