首页> 外文期刊>International Review of Aerospace Engineering >Simultaneous Control of Vortex-Sizes Around Spike Root and Body Base for a Blunt-Nosed Cylindrical Body
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Simultaneous Control of Vortex-Sizes Around Spike Root and Body Base for a Blunt-Nosed Cylindrical Body

机译:尖头圆柱体同时控制尖峰根部和体基周围的涡流大小

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摘要

Forward-facing spike has been identified as a passive flow control technique to render the strong pressure envelope at the nose to become weaker, thereby resulting in reduced pressure over the nose, as a consequence of vortices positioned at the root end, leading to drag reduction. Attention is focused on understanding this aspect of the flow process at low Reynolds number (incompressible flow). It is known that the vortices at the attached end of the spike are responsible for reducing the high-pressure over the nose, leading to drag reduction. In this research, it has been observed that these vortices at the root of the spike would also influence the vortices (wake-expanse) at the base. It would be of great significance for drag reduction if the functional dependence of the size of these vortices (spike-root as well as wake) on spike characteristics can be established. Therefore, in this study, emphasis is focused on ascertaining the simultaneous dependence of the size of the vortices, at the root end of the spike and at the base of the body, on the flow Reynolds number and spike-nose geometry. This had been achieved by visualizing the flow past a blunt-nose body with and without spike at Reynolds number 3170. It is found that there exists a specific length-to-diameter ratio for every spike nose-configuration, resulting in the largest vortex both at the spike base and at body base, leading to significant reduction of drag.
机译:前向尖峰已被确认为一种被动流量控制技术,可使鼻子处的强压力包络变得更弱,从而由于位于根端的涡流而导致鼻子上的压力降低,从而导致阻力减小。注意集中在了解低雷诺数(不可压缩流动)下流动过程的这一方面。众所周知,尖钉附接端的涡旋负责降低机头上的高压,从而降低阻力。在这项研究中,已经观察到尖峰根部的这些涡流也会影响基部的涡流(尾波扩展)。如果可以确定这些旋涡的大小(尖峰根和尾流)对尖峰特性的功能依赖性,那么对于减小阻力将具有重要意义。因此,在这项研究中,重点集中在确定旋涡的大小(在尖峰的根端和身体的底部)对流雷诺数和尖峰鼻几何形状的同时依赖性。这是通过可视化流经带有和不带有雷诺数为3170的尖峰的钝鼻体的流动来实现的。发现每个尖峰鼻形结构都有特定的长径比,这导致了最大的涡旋在长钉底部和身体底部,从而显着减少阻力。

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