燃油喷嘴内非定常空化流动及冲蚀的计算研究

Javad Hosseinpour, L. Bravo, O. Samimi-Abianeh
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引用次数: 6

摘要

剪切驱动空化在许多技术应用中起着重要作用,包括喷油器和发电机。空化影响组件的性能,因此理解和预测其行为是可取的,因为它可以有有利的和不利的后果。虽然已经有大量的研究,但还没有一个完整的认识或描述其行为的理论框架。这部分是由于空化流动的复杂性,包括内部流动物理、湍流、两相流和非平衡热力学。此外,实验技术在以足够的分辨率可视化现象以进行详细分析方面受到限制。本文采用非结构化、有限体积、计算流体动力学(CFD)程序与欧拉-欧拉多流体模型耦合,研究了喷管内的空化现象。在ΔP = 20、40、60、70、75、80和85 bar的一系列条件下,Winkhlofer喷嘴已被广泛报道,并使用正十二烷基准燃料特性进行建模。对三种空化子模型进行了研究,并将结果与以往的实验和模拟流动数据进行了比较。采用Reynolds平均Navier - Stokes方程(RANS)和大涡模拟(LES)模型对湍流流场进行了模拟,并对模拟结果进行了评价。网格灵敏度分析采用13.40 μm、9.48 μm、7.55 μm和6.13 μm的最小网格尺寸显示网格收敛性。此外,还集成了一种新的侵蚀模型,以识别与喷嘴流动操作条件相关的潜在脆弱性损伤区域。计算结果与光学喷嘴的实验数据和前人的模拟结果吻合较好。该模型捕获了固体边界附近的空化现象,能够预测临界空化现象和阻塞流区域。这与所有的模型一致。侵蚀模型的结果显示,表面侵蚀与平均渗透深度(MDPR)和孵育时间之间存在直接关系,喷嘴上的压降更高。这些发现有助于未来喷油器喷嘴的设计,以更好地减轻空化引起的材料损伤,从而提高发动机的耐久性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Computational Study of Unsteady Cavitating Flows and Erosion in a Fuel Nozzle
Shear-driven cavitation plays an important role in many technological applications, including fuel injectors and power generators. Cavitation affects the performance of components and hence it is desirable to understand and predict its behavior since it can have favorable as well as adverse consequences. Although there have been a vast number of studies, a full understanding or theoretical framework describing its behavior has not yet been achieved. This is in part due to the complexities associated with cavitating flows including, internal flow physics, turbulence, two-phase flow and non-equilibrium thermodynamics. Further, experimental techniques are limited in their ability to visualize the phenomena with sufficient resolution for a detailed analysis. In this work, an unstructured, finite volume, computational fluid dynamic (CFD) code coupled to the Eulerian-Eulerian multi-fluid model is utilized to study cavitation phenomena in a nozzle. The well-reported Winkhlofer nozzle at a range of conditions including ΔP = 20, 40, 60, 70, 75, 80, and 85 bar is modeled using n-dodecane reference fuel properties. Three cavitation sub-models were investigated and the results compared with previous experimental and simulation flow data. The flow turbulence was modeled using Reynolds Averaged Navier Stokes Equation (RANS) and Large Eddy Simulation (LES) models and the results evaluated. A mesh sensitivity analysis was conducted with minimum cell sizes of 13.40, 9.48, 7.55, and 6.13 μm were considered to show grid convergence. Further, a novel erosion model was also integrated to identify the potential vulnerability damage zones with respect to the nozzle flow operating conditions. The results were in good agreement with experimental data from optical nozzles as well as previous simulation results. The models capture the cavitation near the solid boundary region and were able to predict the critical cavitation as well as the chocked flow regions. This was consistent with all the models. The results from the erosion model revealed a direct relationship between surface erosion, in terms of Mean Depth of Penetration Rate (MDPR) and incubation time, to higher pressure drops across the nozzle. These findings can be useful to develop future injector nozzle designs that can better mitigate cavitation induced material damage for improved engine endurance.
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