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Visualization of burning flow around a ram accelerator projectile by coaxial simultaneous shadow/direct photography

机译:通过同轴同步阴影/直接摄影可视化冲压加速器弹丸周围的燃烧流

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Experimental investigations with flow visualization of a ram accelerator are reported. The ram accelerator at Hiroshima University uses a tube with a rectangular cross section and a two-dimensional projectile. Observation windows installed on the flat wall of the rectangular tube enable visualization of the flow field around the projectile. In addition to the instantaneous shadow photography method conventionally used for visualization, a direct photography method has been introduced. This direct photography can detect the precise position and brightness of combustion that cannot be observed by shadowgraph. The experiments were conducted at various projectile velocities in the thermally choked mode. The propellant mixture is stoichiometric methane-oxygen diluted by carbon dioxide. It is observed that a tiny flamelet, assumed to be the remains of the starting process, adheres to the projectile forebody, however, visible light emission could not be detected there by direct photography. The brightest emission from combustion is observed around the rear of the projectile, and strong emission is found in the boundary layer on the surface of the projectile afterbody and at the center of the tube behind the projectile. It is also found that the gas mixture is burned over a shorter distance when the projectile moves more slowly. [References: 18]
机译:报道了具有柱塞加速器的流动可视化的实验研究。广岛大学的ram加速器使用具有矩形横截面和二维弹丸的管。安装在矩形管平壁上的观察窗可显示弹丸周围的流场。除了通常用于可视化的瞬时阴影摄影方法之外,还引入了直接摄影方法。这种直接摄影可以检测出阴影图无法观察到的精确的燃烧位置和亮度。实验是在各种射弹速度下以热阻模式进行的。推进剂混合物是被二氧化碳稀释的化学计量的甲烷-氧气。可以观察到,假定是起始过程的剩余部分的微小火焰附着在弹丸前体上,但是,直接摄影无法检测到可见光。在弹丸的后部周围观察到燃烧产生的最亮的发射,并且在弹丸后身表面的边界层和弹丸后面的管中心发现了强发射。还发现,当弹丸移动得更慢时,气体混合物会燃烧更短的距离。 [参考:18]

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