The Study by Visualization of Vortex Structures on a Warhead Wing,Apex Angle (Ã)=68.6°

A. Abderrahmane
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引用次数: 1

Abstract

This study has been given prominence and confirmed by extensive documentation while recent visualizations observed in a wind tunnel have revealed that rectilinear vortex flows from different angles interacting with one another above warheads. My experimental research has indicated the many and very specific series, by visualizations of wisps of smoke trails, of vortex structures of a preferential nature above a warhead where β=68.6°. The positioning of those structures has thus been determined with regard to the application of very general criteria governing the stability of vortex flows. What have also been exposed are the specific aspects of vortex flows together with some comments concerning the bursting of vortices above the warhead. The purpose of this study is to optimize the connection between marine, air and land forms such as sails, the wings of aircraft, cars and trains – and the stability of fluid flows around such forms.
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战斗部机翼涡结构的可视化研究,顶点角(Ã)=68.6°
这项研究已经得到了重视,并得到了大量文献的证实,而最近在风洞中观察到的可视化结果显示,在弹头上方,不同角度的直线涡旋流动相互作用。我的实验研究表明了许多非常具体的系列,通过缕缕烟雾痕迹的可视化,在β=68.6°的弹头上方具有优先性质的漩涡结构。因此,这些结构的位置是根据控制旋涡流动稳定性的非常一般的标准的应用来确定的。还暴露了旋涡流动的具体方面,以及有关弹头上方旋涡破裂的一些评论。这项研究的目的是优化海洋、空中和陆地形态(如船帆、飞机机翼、汽车和火车)之间的联系,以及这些形态周围流体流动的稳定性。
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