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首页> 外文期刊>International Journal of Spray and Combustion Dynamics >Liquid jet breakup unsteadiness in a coaxial air-blast atomizer
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Liquid jet breakup unsteadiness in a coaxial air-blast atomizer

机译:同轴风爆雾化器中的液体喷射分解不稳定

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The aim of this paper is to experimentally characterize the liquid jet breakup unsteadiness in a coaxial air-blast atomizer. The current research focuses on the measurement of the fluctuations of the jet breakup length and the flapping instability of the liquid jet, which contribute to the downstream fluctuations of the spray characteristics. The optical connectivity technique was used to measure the instantaneous breakup length of the water jet. Also, time resolved shadowgraph images of the primary jet breakup process were captured by high-speed imaging to characterize the jet instabilities at different axial locations from the atomizer exit. Experiments were performed for a wide range of air-to-liquid momentum flux ratio (M) and aerodynamic Weber number (We(g)) corresponding to membrane- and/or fiber breakup mode of the jet disintegration process. The mean jet breakup length was found to vary inversely with M through a power law relation in agreement with the literature, while the breakup length fluctuations were found to first decrease and then increase with M. In order to capture the unsteady dynamics of the jet breakup process, the proper orthogonal decomposition analysis of the optical connectivity images was performed. The jet flapping and the fluctuations of the jet breakup length were identified as the second and the third spatial proper orthogonal decomposition modes, respectively, for all operating conditions of the atomizer. The amplitude and the frequency of the instabilities were measured by temporal tracking of the liquid-air interface on the shadowgraph images. The disturbance close to the injector exit corresponds to the Kelvin-Helmholtz instability, while close to the jet breakup point the jet exhibits the flapping instability, which is characterized by lateral oscillation of the jet about the atomizer axis. The influence of the liquid jet Reynolds number and momentum flux ratio on the KH and the flapping instabilities are examined.
机译:本文的目的是通过实验表征同轴风吹雾化器中的液体喷射破碎污染。目前的研究侧重于测量喷射分解长度的波动和液体射流的扑置不稳定,这有助于喷射特性的下游波动。光学连接技术用于测量水射流的瞬时分解长度。而且,通过高速成像来捕获一次分辨的主喷射过程的影子图像,以表征来自雾化器出口的不同轴向位置的喷射不置于。对应于射流崩解过程的膜和/或纤维分解模式,对对应于膜 - 和/或纤维分解模式进行的实验进行实验。发现平均喷射长度通过与文献一致的权力律关系相同,同时发现分手长度波动首先减少,然后用M增加。为了捕获喷射分析的不稳定动态。过程中,执行光学连接图像的适当正交分解分析。射流凸起和喷射分解长度的波动分别被识别为第二和第三空间适当的正交分解模式,用于雾化器的所有操作条件。通过向影片图图像上的液体空气接口的时间跟踪来测量稳定性的幅度和频率。接近喷射器出口的扰动对应于Kelvin-Helmholtz不稳定性,而近射射流啮合射流表现出凸起的不稳定性,其特征在于射雾围绕雾化器轴的横向振荡。研究了液体射流雷诺数和动量磁通比对KH和扑振不稳定性的影响。

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