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Effects of Orifice Geometry on Spray Characteristics of Impinging Jet Injectors for Gelled Propellants

机译:孔口几何形状对胶凝推进剂撞击射流喷射器喷雾特性的影响

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This paper presents the results of an experimental study on breakup characteristics of gelled propellant liquid sheets formed by impinging jet injectors with different geometries of injector orifice (round, elliptic, and rectangular shape). Spray formation of gelled propellant from impinging jet injectors was described by carrying out experiments in a spray test facility. Considering the safety, a water based gel simulant was used instead of the gelled propellant in the experiments. The Theological characteristics of the gel simulant were tested. A high speed camera was used to grab the detailed information of the liquid sheet breakup process and spray development. The experiments were performed with injectors of different shape of injector orifice to test the geometrical effect of injector orifice on the spray characteristics. The experimental results showed that under the condition of identical sectional area, the shapes of liquid sheet formed by the impinging jet injectors with different shape of orifices were different. One special phenomenon is the thick liquid stream in the center of liquid sheet when the aspect ratio of rectangular orifice is great. The reason of this phenomenon is the axis-switching feature of the non-circular jets. The mass flow rates of square and elliptical orifices are larger than that of circular orifice. The flow rate of rectangular orifice becomes greater as the aspect ratio gets larger. The breakup length for injector with square orifice is shorter than that for injector with circular orifice. Although the elliptical jet behaves greater instability than circular jet, the liquid sheet breakup length of injector with elliptical orifice is not always shorter than that of injector with circular orifice. Generally, the breakup length of rectangular jet impinging injector increases with aspect ratio.
机译:本文介绍了通过对具有不同几何形状的喷射器孔(圆形,椭圆形和矩形)的喷射式喷射器进行撞击而形成的胶状推进剂液体薄片破裂特性的实验研究结果。通过在喷雾测试设备中进行实验,描述了撞击喷射器形成胶凝推进剂的喷雾形成。考虑到安全性,在实验中使用水基凝胶模拟剂代替凝胶化推进剂。测试了凝胶模拟物的神学特性。使用高速摄像头获取液膜破裂过程和喷雾形成的详细信息。用不同形状的喷射器孔进行喷射实验,以测试喷射器孔对喷雾特性的几何影响。实验结果表明,在相同的截面积条件下,具有不同孔口形状的撞击式喷射器形成的液体片的形状是不同的。一种特殊的现象是,当矩形孔的长径比很大时,液膜中心的液体流就很浓。这种现象的原因是非圆形射流的轴切换特性。方形和椭圆形孔口的质量流率大于圆形孔口的质量流率。长宽比越大,矩形孔的流量越大。具有方形孔口的喷射器的破裂长度比具有圆形孔口的喷射器的破裂长度短。尽管椭圆形射流比圆形射流具有更大的不稳定性,但是具有椭圆形孔口的喷射器的液膜破裂长度并不总是比具有圆形孔口的喷射器的液膜破裂长度短。通常,矩形喷射冲击喷射器的破裂长度随长宽比而增加。

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