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首页> 外文期刊>International journal of engine research >Spray characterization for engine combustion network Spray G injector using high-fidelity simulation with detailed injector geometry
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Spray characterization for engine combustion network Spray G injector using high-fidelity simulation with detailed injector geometry

机译:用高保真仿真,用高保真仿真喷射发动机燃烧网络喷射器的喷涂特性

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摘要

This article presents a computational fluid dynamics study of the engine combustion network Spray G, focusing on the transient characteristics of the spray during the start of injection and the impacts of nozzle geometry details derived from the manufacturing process. The large-eddy-simulation method, coupled with the volume-of-fluid method, was used to model the high-speed turbulent two-phase flow. A moving-needle boundary condition was applied to capture the internal flow boundary condition accurately. The injector geometry was measured with micron-level resolution using X-ray tomographic imaging at the Advanced Photon Source at Argonne National Laboratory, providing detailed machining tolerance and defects from manufacturing and a realistic rough surface. For comparison, a nominal geometry and a modified geometry incorporating measured large-scale geometric features but no surface details were also used in the simulations. Spray characteristics such as mass flow rate, injection velocity, and Sauter mean diameter were analyzed. Significantly distinct spray characteristics in terms of injection velocity, spray morphology, and primary breakup mechanism were predicted using different nozzle geometries, which is mainly attributable to the realistic surface finish and manufacturing defects. The measured high-resolution geometry predicts a lower injection velocity, a wider-spreading spray, and an overall slower breakup rate with evident injector tip wetting compared to the ideally smooth nozzle boundary. This result implies that the manufacturing details of the injector, which are usually ignored in fuel injection studies, have a significant impact on the spray development process and should be taken into account for design optimization.
机译:本文介绍了发动机燃烧网络喷射G的计算流体动力学研究,该研究专注于喷射开始期间喷射的瞬态特性以及喷嘴几何细节从制造过程中产生的影响。耦合与流体体积方法的大涡流模拟方法用于建模高速湍流两相流。施加移动针边界条件以精确地捕获内部流边界条件。使用在Argonne National实验室的高级光子源的X射线层压成像用微米级分辨率测量喷射器几何体,从argonne国家实验室提供详细的加工公差和制造的缺陷和逼真的粗糙表面。为了比较,标称几何和改进的几何形状,其具有测量的大规模几何特征,但在模拟中也没有表面细节。分析了诸如质量流量,注射速度和燃烧器平均直径的喷雾特性。使用不同的喷嘴几何形状预测了在注射速度,喷雾形态和初级分解机构方面显着不同的喷射特性,主要是归因于现实表面光洁度和制造缺陷的原因。测量的高分辨率几何形状预测较低的注射速度,更宽的扩散喷雾,以及与理想光滑的喷嘴边界相比,具有明显的喷射器尖端润湿的整体较慢的分离速率。该结果意味着,通常在燃料喷射研究中忽略的喷射器的制造细节对喷雾开发过程产生了重大影响,并且应考虑到设计优化。

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