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Effect of Backpressure on Internal Flow Dynamics and Spray Characteristics of Liquid Swirl Injector

机译:背压对液体旋流器内部流动动力学和喷雾特性的影响

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A combined theoretical and numerical analysis was performed to explore the flow characteristics in liquid swirl injectors under a wide range of backpressure. Axial velocity in nozzle, surface wave speed and spray pattern were theoretically studied basing on existing theories. Numerical simulations basing on swirl axi-symmetric model were carried on by solving of the Navier-Stokes equations coupled with the VOF equation implemented with CICSAM surface tracking technique on adapted grids. The effects of inlet turbulent intensity and backpressure to the film thickness were investigated by analyzing the velocity component profiles. The results showed that it is the changes of velocity profiles caused by increased gas shear stresses following increased backpressure responses to the increasing to film thicknesses. Using a long nozzle makes this simulation study have the ability to catch the stationary surface wave which was not well investigated before. Mechanism of wave generation was explained by analogy with the classical gravity wave theories. The effects of backpressure to spraying cone of liquid swirl injector were also studied by combining theory with numerical simulation. It showed that the increasing pressure different between internal and external surface of spraying cone caused contraction. A model of spray patterns was established by relating pressure different to the velocity at surface of liquid sheet and showed a good agreement with experiment results.
机译:进行了理论和数值分析的组合,以探索在宽背压范围内液体旋流喷射器中的流动特性。在现有理论的基础上,对喷嘴的轴向速度,表面波速度和喷射方式进行了理论研究。通过求解Navier-Stokes方程以及结合CICSAM表面跟踪技术在自适应网格上实现的VOF方程,进行了基于旋涡轴对称模型的数值模拟。通过分析速度分量分布,研究了入口湍流强度和背压对薄膜厚度的影响。结果表明,这是由于背压对膜厚的增加而引起的气体剪切应力增加所引起的速度分布的变化。使用长喷嘴使此模拟研究具有捕获以前未进行充分研究的固定表面波的能力。通过与经典重力波理论的类比解释了波浪产生的机理。将理论与数值模拟相结合,研究了背压对液体旋流喷油器喷淋锥的影响。结果表明,喷射锥内外表面压力的增加引起收缩。通过将与液体表面速度不同的压力联系起来,建立了喷雾模式的模型,表明与实验结果吻合良好。

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