Les Study of Injector Geometry and Parcel Injection Location on Spray Simulation of The Ecn Spray G Injector

IF 1.4 4区 工程技术 Q3 ENGINEERING, MECHANICAL Journal of Engineering for Gas Turbines and Power-transactions of The Asme Pub Date : 2023-11-02 DOI:10.1115/1.4063957
Aman Kumar, Justin A Boussom, Noah Van Dam
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Abstract

Abstract Recent improvements in computing power and numerical techniques have enabled us resolve minute details of spray plume behavior and its wall boundary interactions, and made detailed spray simulations using Large-eddy Simulation (LES) turbulence models available to many more engineers. However, guidelines for parcel-based spray simulation boundary and initial conditions are still based on results from lower-resolution and Reynolds Averages Navier-Stokes (RANS) simulations. Hence, it is necessary to critically examine those assumptions and compare their impact with results using a RANS turbulence model. Three different parameters, including whether a simulation includes a detailed injector tip geometry or a flat surface, whether parcels are initialized at the counterbore exit, which is more common, or at the nozzle exit, and whether to use an experimentally derived rate of injection or one-way coupling with a separate internal nozzle Volume of Fluid simulation, were examined with an LES turbulence model. Both local data close to the injector and global penetration results were used to compare simulations. Local data, such as the local liquid volume fraction, showed greater variation between the conditions, which may have an impact on mixing and combustion predictions in engine applications. Spray penetration and other global measures demonstrated limited sensitivity to the boundary conditions/initialization procedure. Results were also compared with prior results that used a RANS turbulence model. RANS simulations had overall smoother responses to the changes, as would be expected, but LES simulations showed similar trends in the effects for the measured variables.
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Ecn Spray G喷油器喷雾模拟中喷油器几何形状和包注位置的研究
最近计算能力和数值技术的改进使我们能够解决喷流行为及其壁面边界相互作用的微小细节,并使更多的工程师可以使用大涡模拟(LES)湍流模型进行详细的喷雾模拟。然而,基于包裹的喷雾模拟边界和初始条件的指导方针仍然基于低分辨率和Reynolds平均Navier-Stokes (RANS)模拟的结果。因此,有必要严格检查这些假设,并将其影响与使用RANS湍流模型的结果进行比较。通过LES湍流模型,研究了三个不同的参数,包括模拟是否包括详细的喷油器尖端几何形状或平面,包裹是在反孔出口初始化(更常见)还是在喷嘴出口初始化,以及是使用实验推导的喷射速率还是与单独的内部喷嘴单向耦合流体模拟体积。使用靠近注入器的局部数据和全局穿透结果来比较模拟结果。局部数据,如局部液体体积分数,在不同条件下差异较大,这可能对发动机应用中的混合和燃烧预测产生影响。喷雾渗透和其他全局测量表明,对边界条件/初始化程序的敏感性有限。结果还与先前使用RANS湍流模型的结果进行了比较。正如预期的那样,RANS模拟对变化的总体响应更平滑,但LES模拟对测量变量的影响显示出类似的趋势。
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来源期刊
CiteScore
3.80
自引率
20.00%
发文量
292
审稿时长
2.0 months
期刊介绍: The ASME Journal of Engineering for Gas Turbines and Power publishes archival-quality papers in the areas of gas and steam turbine technology, nuclear engineering, internal combustion engines, and fossil power generation. It covers a broad spectrum of practical topics of interest to industry. Subject areas covered include: thermodynamics; fluid mechanics; heat transfer; and modeling; propulsion and power generation components and systems; combustion, fuels, and emissions; nuclear reactor systems and components; thermal hydraulics; heat exchangers; nuclear fuel technology and waste management; I. C. engines for marine, rail, and power generation; steam and hydro power generation; advanced cycles for fossil energy generation; pollution control and environmental effects.
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