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Investigation of the impact of high liquid viscosity on jet atomization in crossflow via high-fidelity simulations

机译:高保真仿真对高液粘度对跨流量喷射雾化影响的研究

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摘要

0 Atomization of extremely high viscosity liquid can be of interest for many applications in aerospace, automotive, pharmaceutical, and food industries. While detailed atomization measurements usually face grand challenges, high-fidelity numerical simulations offer the advantage to comprehensively explore the atomization details. In this work, a previously validated high-fidelity first-principle simulation code HiMIST is utilized to simulate high-viscosity liquid jet atomization in crossflow. The code is used to perform a parametric study of the atomization process in a wide range of Ohnesorge numbers (Oh = 0.004-2) and Weber numbers (We = 10-160). Direct comparisons between the present study and previously published low-viscosity jet in crossflow results are performed. The effects of viscous damping and slowing on jet penetration, liquid surface instabilities, ligament formation/breakup, and subsequent droplet formation are investigated. Complex variations in near-field and far-field jet penetrations with increasing Oh at different We are observed and linked with the underlying jet deformation and breakup physics. Transition in breakup regimes and increase in droplet size with increasing Oh are observed, mostly consistent with the literature reports. The detailed simulations elucidate a distinctive edge-ligament-breakup dominated process with long surviving ligaments for the higher Oh cases, as opposed to a two-stage edge-stripping/column-fracture process for the lower Oh counterparts. The trend of decreasing column deflection with increasing We is reversed as Oh increases. Apredominantly unimodal droplet size distribution is predicted at higher Oh, in contrast to the bimodal distribution at lower Oh. It has been found that both Rayleigh-Taylor and Kelvin-Helmholtz linear stability theories cannot be easily applied to interpret the distinct edge breakup process and further study of the underlying physics is needed. Published by AIP Publishing.
机译:0极高粘度液体的雾化对于航空航天,汽车,制药和食品工业中的许多应用可能感兴趣。虽然详细的雾化测量通常面临大挑战,但高保真数值模拟提供了全面探索雾化细节的优势。在这项工作中,利用以前验证的高保真的第一原理模拟代码来模拟横流的高粘度液体喷射雾化。该代码用于在广泛的OHNESORGLE数字(OH = 0.004-2)和Weber号码(WE = 10-160)中执行参数化雾化过程的参数研究。进行本研究与先前公布的低粘度射流在横流结果之间的直接比较。研究了粘性阻尼和减速对喷射渗透,液体表面稳定性,韧带形成/分解和随后的液滴形成的影响。观察到近场近场和远场喷射渗透的复杂变化,并与底层喷射变形和分离物理相连。观察到在分手制度和液滴尺寸随着较高oh的增加而增加,主要与文献报告一致。详细仿真阐明了具有长度存活的韧带的独特的边缘韧带分发的过程,其对于较高的OH壳体,而不是较低OH对应物的两级边缘剥离/柱裂过程。随着越来越多的情况下,随着oh增加,我们越来越越来越多地逆转。与较低oh的双峰分布相比,预先预测纯净的单峰液滴尺寸分布。已经发现,Rayleigh-Taylor和Kelvin-Helmholtz线性稳定性理论不能容易地应用于解释独特的边缘分析过程,并且需要进一步研究潜在物理学。通过AIP发布发布。

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  • 来源
    《Physics of fluids》 |2017年第8期|共17页
  • 作者单位

    United Technol Res Ctr E Hartford CT 06108 USA;

    United Technol Res Ctr E Hartford CT 06108 USA;

    United Technol Res Ctr E Hartford CT 06108 USA;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 流体力学;
  • 关键词

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