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首页> 外文期刊>Journal of Aircraft >Forebody Geometry Effects on the Flowfield of a Blunt-Nose Projectile at High Alpha
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Forebody Geometry Effects on the Flowfield of a Blunt-Nose Projectile at High Alpha

机译:前体几何形状对高阿尔法钝鼻炮弹流场的影响

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摘要

Wind-tunnel experiments are conducted on a projectile at high incidence to examine the effect of nose shapes and a passive strake control device on the side force and yawing moment. The study was also aimed at gaining some insights into the fluid mechanics of blunt-nose bodies of revolution at high angles of attack. Detailed flow visualization and force measurements are obtained on a projectile with a fineness ratio of 4 at a Reynolds number of 0.19 × 10~6 and 42-and 48-deg angles of attack. Off- and on-surface flow visualization records are collected to study the effects of two blunt noses: a hemispherical nose and an elliptical nose with 33% ellipticity. It was found that the elliptical nose results in flow behaviors typical of a blunt nose, whereas the hemispheric nose results in behaviors that are akin to a pointed nose. An explanation for the contrasting behaviors is provided.
机译:在高射速弹丸上进行风洞实验,以检查机头形状和被动式行进控制装置对侧向力和偏航力矩的影响。该研究的目的还在于获得对高攻角钝头旋转体的流体力学的一些见解。详细的流动可视化和力测量是在细度比为4的弹丸上获得的,雷诺数为0.19×10〜6,攻角为42度和48度。收集了表面和表面上的流动可视化记录,以研究两个钝鼻子的影响:半球形鼻子和椭圆率为33%的椭圆鼻子。已经发现,椭圆形的鼻子导致了典型的钝鼻子流动行为,而半球形的鼻子导致了类似于尖鼻子的行为。提供了对比行为的说明。

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