Influence of Reactor Pressure on the Primary Jet Breakup of High-Viscosity Fuels: Basic Research for Simulation-Assisted Design of Low-Grade Fuel Burner

T. Müller, Kathrin Kadel, P. Habisreuther, D. Trimis, N. Zarzalis, A. Sänger, T. Jakobs, T. Kolb
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引用次数: 1

Abstract

Detail investigations on the primary breakup of high-viscosity liquids using external-mixing twin-fluid nozzles at increased system pressure are scarce. Therefore, the research work of the present study is focused on the investigation of pressure influence (1 - 11 bar (abs)) on the primary breakup by numerical simulation based on a previously studied nozzle [Müller et al., ASME Turbo Expo 2016, GT2016-56371]. The pressure influence was investigated for two liquids applying a wide range of viscosities (100 mPa s; 400 mPa s) and two atomizing air velocities (58 m/s; 74 m/s). To describe the disintegration process of the fluids, characteristic features like liquid jet morphology, breakup length and breakup frequency were evaluated. The primary breakup was investigated using the open source CFD software OpenFOAM. To gather the morphology of the primary breakup and the flow field characteristics compressible large eddy simulations (LES) were performed and the movement of the gas-liquid interface was captured by means of the Volume of Fluid-Method (VOF). The conducted simulations showed good agreement with experimental results with respect to the characteristic features (e.g. morphology and breakup length) and revealed a decrease of the breakup length with increasing ambient pressure for a constant liquid mass flow and atomizing air velocity. Moreover, those findings will contribute to a better understanding of the physics of the breakup of high-viscosity liquid jets and as well to create an experimentally validated CFD based tool for future burner development and optimization.
反应器压力对高粘度燃料一次射流破碎的影响——低品位燃料燃烧器模拟辅助设计的基础研究
在系统压力增加的情况下使用外混合双流体喷嘴对高粘度液体进行初次破碎的详细研究很少。因此,本研究的研究工作主要集中在基于先前研究的喷嘴的数值模拟研究压力(1 - 11 bar (abs))对初级破裂的影响[m ller等,ASME Turbo Expo 2016, GT2016-56371]。研究了两种粘度范围较大的液体(100mpa s;400 mPa /s)和两个雾化风速(58 m/s;74米/秒)。为了描述流体的解体过程,对射流形态、破裂长度和破裂频率等特征进行了评价。使用开源CFD软件OpenFOAM对初次破裂进行了研究。为了获得初次破裂的形态和流场特征,进行了可压缩大涡模拟(LES),并利用流体体积法(VOF)捕捉了气液界面的运动。模拟结果与实验结果吻合较好,在液体质量流量和雾化气流速度恒定的情况下,随着环境压力的增加,破裂长度减小。此外,这些发现将有助于更好地理解高粘度液体射流破裂的物理原理,并为未来燃烧器的开发和优化创建一个实验验证的基于CFD的工具。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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