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Numerical Investigation of the Flow Dynamics Inside Supersonic Fluid Ejector

机译:超声流体喷射器内部流动动力学的数值研究

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This paper describes the flow dynamics inside a supersonic ejector using CFD modelling. Suitable ejector geometry isproposed for the high compression ratios encountered in real-world applications. Post-processing and physical analysis ofthe CFD results are presented to better understand the entrainment mechanism and the mixing between the primary andthe secondary fluids. The effect of the primary pressure on the flow dynamics and the entrainment ratio is discussed for thetwo compression ratios of 1.67 and 3.4. It is found that the proposed ejector can operate at compression ratio as high as 3.4.It is also found that the strength of the shock waves, the supersonic jet expansion and the mixing between the primary andsecondary fluid flows inside the ejector are strongly affected by the primary pressure. A significant increase in both the shearforces amplitude and the wall friction losses is observed when the boundary layer separates from the ejector wall.
机译:本文使用CFD建模技术描述了超音速喷射器内部的流动动力学。针对现实应用中遇到的高压缩比,提出了合适的喷射器几何形状。提出了CFD结果的后处理和物理分析,以更好地理解夹带机理以及一次和二次流体之间的混合。对于1.67和3.4的两个压缩比,讨论了主压力对流动动力学和夹带率的影响。结果发现拟议的喷射器可以在高达3.4的压缩比下工作,还发现冲击波的强度,超音速射流膨胀以及喷射器内部的一次,二次流体之间的混合受到强烈的影响。初级压力。当边界层与喷射器壁分离时,可观察到剪切力振幅和壁摩擦损耗的显着增加。

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