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首页> 外文期刊>The Journal of Computational Multiphase Flows >Numerical Analysis of the Primary Breakup Applying the Embedded DNS Approach to a Generic Prefilming Airblast Atomizer
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Numerical Analysis of the Primary Breakup Applying the Embedded DNS Approach to a Generic Prefilming Airblast Atomizer

机译:嵌入式DNS方法应用于通用预成膜爆破雾化器的一次分解的数值分析

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An improved understanding of the breakup processes of two-phase flows is essential to effectively control the fuel atomization for future aircraft engines. A detailed insight into the phenomena of primary breakup is a major limitation in gaining this knowledge. Aircraft engines use airblast atomizers to provide the fuel atomization. The geometries of airblast atomizers are complex, the operating conditions are characterized by high Reynolds- and Weber numbers. Direct Numerical Simulations (DNS) of liquid breakup under realistic conditions and geometries are hardly possible. The embedded DNS (eDNS) concept aims to fill this gap. The concept consists of three steps: a geometry simplification, the generation of realistic boundary conditions for the DNS and the DNS of the breakup region. The realistic annular airblast atomizer geometry is simplified to a planar geometry. Inside this domain the eDNS is located. The eDNS domain requires the generation of boundary conditions. A zonal Large Eddy Simulation (LES) of the turbulent channel flow is performed prior to the DNS. The parameters are stored transiently on the "virtual" DNS inlet planes. These variables are then mapped to the DNS. The Volume of fluid (VOF) method is used to solve for the two-phase flow. DNS are performed for a shear-driven liquid wall film and for a generic planar prefilming airblast atomizer. As the Reynolds and Weber number for the first operating point (OP) are low (Re_(air) = 5, 333/We_(film) = 1.9), the liquid wall film as well as the liquid sheet show no surface waves. For the second case with Reair = 13, 333 and We_(film) = 11.9, the surface appears more wrinkled and streamwise waves are transported along the wall for the shear-driven wall film. Instantaneous snapshots in 2-D and 3-D illustrate the qualitative behavior of the liquid sheet in time. Leaving the prefilmer trailing edge, the liquid sheet starts to oscillate in a sinusoidal fashion. This oscillation appears crucial for the onset of primary breakup. The qualitative characterization of the breakup for OP 1 and OP 2, yield to the distinction of the stretched ligament breakup for the former, and the torn-sheet breakup for the latter OP. The breakup time for OP 1 is longer than for OP 2. This study proves the applicability of the eDNS concept for investigating breakup processes as the transient nature of the phase interface behavior can be captured. The approach offers the potential of simulating realistic annular highly-swirled airblast atomizer geometries under realistic conditions.
机译:更好地理解两相流的分解过程对于有效控制未来飞机发动机的燃料雾化至关重要。对初次破裂现象的详细了解是获得该知识的主要限制。飞机发动机使用鼓风雾化器来提供燃料雾化。鼓风雾化器的几何形状复杂,运行条件​​的特点是雷诺数和韦伯数高。在实际条件和几何条件下,液体破碎的直接数值模拟(DNS)几乎是不可能的。嵌入式DNS(eDNS)概念旨在填补这一空白。该概念包括三个步骤:简化几何结构,为DNS和分解区域的DNS生成实际边界条件。实际的环形鼓风雾化器几何形状简化为平面几何形状。在此域中,已找到eDNS。 eDNS域要求生成边界条件。在DNS之前执行湍流通道流的区域大涡模拟(LES)。参数被临时存储在“虚拟” DNS入口平面上。然后将这些变量映射到DNS。流体体积(VOF)方法用于求解两相流。 DNS用于剪切驱动的液体壁膜和通用的平面预成膜鼓风雾化器。由于第一工作点(OP)的雷诺数和韦伯数较低(Re_(空气)= 5,333 / We_(膜)= 1.9),因此液壁膜和液膜均无表面波。对于Reair = 13、333和We_(film)= 11.9的第二种情况,表面出现了更多的褶皱,并且沿着剪切驱动壁膜的壁传输了水流。 2-D和3-D中的瞬时快照说明了液膜随时间的定性行为。离开预成膜器的后缘,液体纸开始以正弦形式振荡。这种振荡似乎对于初次破裂的发作至关重要。 OP 1和OP 2破裂的定性表征可区分前者拉伸韧带破裂和后者OP的撕裂片破裂。 OP 1的断开时间比OP 2的断开时间长。这项研究证明了eDNS概念在研究断开过程中的适用性,因为可以捕获相界面行为的瞬态性质。该方法提供了在现实条件下模拟现实的环形高涡流式鼓风雾化器几何形状的潜力。

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