PDF下载 分享
[1]刘昌波,周立新,雷凡培.雾化过程的数值模拟研究综述[J].火箭推进,2014,40(01):10-17.
　LIU Chang-bo,ZHOU Li-xin,LEI Fan-pei.Overview on numerical simulations of primary atomization[J].Journal of Rocket Propulsion,2014,40(01):10-17.
点击复制

雾化过程的数值模拟研究综述

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 40 期数: 2014年01期 页码: 10-17 栏目: 专论与综述 出版日期: 2014-02-28
Title:
Overview on numerical simulations of primary atomization
作者:
刘昌波1; 周立新1; 雷凡培2
1. 西安航天动力研究所，陕西 西安 710100；2. 中国航天科技集团公司，北京 100037
Author(s):
LIU Chang-bo1;  ZHOU Li-xin1;  LEI Fan-pei2
1. Xi’an Aerospace Propulsion Institute, Xi’an 710100, China; 2. China Aerospace Science and Technology Corporation, Beijing 100037, China
关键词:
雾化过程;  数值模拟; 多尺度仿真; 液滴追踪方法
Keywords:
atomization process;  numerical simulation;  multi-scale simulation;  droplet tracking method
分类号:
V434-34
文献标志码:
A
摘要:
雾化过程的数值模拟主要有3类方法：简单工程模型、准直接数值模拟和多尺度仿真。对这3类方法的基本思想、优缺点和研究应用等情况进行了全面的总结。雾化过程的多尺度仿真，对大块液体的运动采用准直接数值模拟的思想，对小于网格尺度的小液滴采用模型来封闭。这种方法不仅能够反映雾化过程的主要特性，而且计算量适中，已经成为雾化过程数值模拟新的研究方向。
Abstract:
There are three simulation methods for primary atomization: simplified engineering models, DNS (Direct Numerical Simulation)-like simulation and multi-scale simulations. Fundamental ideas, advantages and disadvantages, application status of the three methods are summarized thoroughly in this paper. For the multi-scale simulation method, the blobs larger than the grid volume are captured by the DNS-like method, and those droplets smaller than the grid volume are tracked by simple models. This method can capture the main characteristics of the primary atomization, and its computational cost is moderate. It has become a new research direction for the primary atomization process.

参考文献/References:

[1]REITZ R D. Modeling atomization processes in high- pressure vaporizing sprays[J]. Atomization and Spray Tec- hnology, 1987, 3(4): 309-337.
[2]O'ROURKE P J, AMSDEN A A. The TAB method for numerical calculation of spray droplet breakup, SAE 872089[R]. USA: SAE, 1987.
[3]JIANG X, SIAMAS G A, JAGUS K, et al. Physical mode- ling and advanced simulations of gas-liquid two-phase jet flows in atomization and sprays[J]. Progress in Energy and Combustion Science, 2010, 36(2): 131-167.
[4]KOO J Y. An overview of liquid spray modeling formed by high-shear nozzle/swirler assembly[J]. KSME International Journal, 2003, 17(5): 726-739.
[5]HUU P T, CHEN C P. Modeling of turbulent effects on liquid jet atomization and breakup, AIAA-2005-154[R]. USA: AIAA, 2005.
[6]史春涛, 任立红, 于善颖, 等. 喷雾破碎模型在内燃机CFD中的应用[J]. 拖拉机与农用运输车, 2006, 33(3): 1-4.
[7]VILLIERS E D, GOSMAN A D, WELLER H G. Large eddy simulation of primary diesel spray atomization, SAE 2004-01-0100[R]. USA: SAE, 2004.
[8]CHANG S K, KOO J Y, CHUNG H C. Transient liquid jet breakup model and comparison with phase doppler measurements[J]. KSME International Journal, 1995, 9(1):41-50.
[9]聂万胜, 丰松江. 液体火箭发动机燃烧动力学模型与数值计算[M]. 北京: 国防工业出版社, 2011.
[10]O'ROURKE P J. Collective drop effects on vaporizing liquid sprays[D]. Princeton, New Jersey, USA: Princeton University, 1981.
[11]史春涛, 周颖, 张宝如, 等. 喷雾模型的发展及其在内燃机CFD中的应用[J]. 拖拉机与农用运输车, 2006, 33(2):39-42.
[12]周立新. 同轴离心式气液喷嘴内流场特性研究[D]. 西安: 中国航天科技集团公司第六研究院第十一研究所, 2008.
[13]OSHER S J, SETHIAN J A. Fronts propagating with curvature dependent speed: algorithms based on Hamilton Jacobi formulations[J]. Journal of Computa- tional Physics, 1988, 79(1): 12-49.
[14]MARTINEZ J M, CHENSNEAU X, ZEGHMATI B. A new curvature technique calculation for surface tension contribution in PLIC-VOF method[J]. Computational Mechanics, 2006, 37(2): 182-193.
[15]FUSTER D, BAGUE A, BOECK T, et al. Simulation of primary atomization with an octree adaptive mesh refinement and VOF method[J]. International Journal of Multiphase Flow, 2009, 35(6): 550-565.
[16]YOKOI K. Efficient implementation of THINC scheme: a simple and practical smoothed VOF algorithm[J]. Journal of Computational Physics, 2007, 226(2): 1985-2002.
[17]OLSSON E, KREISS G. A conservative Level Set method for two phase flow[J]. Journal of Computational Physics, 2005, 210(1): 225-246.
[18]DESJARDINS O, MOUREAU V, PITSCH H. An accurate conservative Level Set/Ghost Fluid method for simulating turbulent atomization[J]. Journal of Computational Physics, 2008, 227(18): 8395-8416.
[19]M?魪NARD T, TANGUY S, BERLEMONT A. Coupling level set/VOF/ghost fluid methods: validation and application to 3D simulation of the primary break-up of a liquid jet[J]. International Journal of Multiphase Flow, 2007, 33(5): 510-524.
[20]LEBAS R, MENARD T, BEAU P A, et al. Numerical simulation of primary break-up and atomization: DNS and modeling study[J]. International Journal of Multip- hase Flow, 2009, 35(3): 247-260.
[21]SHINJO J, UMEMURA A. Simulation of liquid jet pri- mary breakup: dynamics of ligament and droplet forma- tion[J]. International Journal of Multiphase Flow, 2010, 36(7): 513-532.
[22]SHINJO J, UMEMURA A. Detailed simulation of primary atomization mechanisms in diesel jet sprays (isolated identification of liquid jet tip effects) [C]// Proceedings of the Combustion Institute. [S.l.]: Elsevier Inc., 2011, 33: 2089-2097.
[23]沃傲波. 柴油机喷雾准直接数值模拟及其雾化机理的研究[D]. 武汉: 华中科技大学, 2007.
[24]ISHIMOTO J, OHIRA K, OKABAYASHI K, et al. Inte- grated numerical prediction of atomization process of liquid hydrogen jet[J]. Cryogenics, 2008, 48(5/6): 238- 247.
[25]GROSSHANS H, SZ?魣SZ R Z, FUCHS L. Full spray si- mulation-coupled volume of fluid and Lagrangian parti- cle tracking methods[C]// Proceedings of 24th European Con- ference on Liquid Atomization and Spray Systems. Esto- ril, Portugal:[s.n.], 2011: 111-121.
[26]KIM D, HERRMAN M, MOIN P. The breakup of a round liquid jet by a coaxial flow of gas using the refined Lev- el Set grid method[C]//Proceedings of 59th Annual Meeting of the APS divisions of Fluid Dynamics. Tampa Bay, FL, USA: University of Florida, 2006: 19-21.
[27]HERRMANN M. A parallel Eulerian interface tracking/Lagrangian point particle multiscale coupling procedure [J]. Journal of Computational Physics, 2010, 229(3): 745-759.
[28]TOMAR G, FUSTER D, ZALESKI S, et al. Multiscale simulations of primary atomization[J]. Computers & Fluids, 2010, 36(10): 1864-1874.
[29]MA D J, CHEN X D, KHARE P, et al. Atomization pat- terns and breakup characteristics of liquid sheets formed by two impinging jets, AIAA-2011-97[R]. USA: AIAA, 2011.
[30]LIU C B, ZHOU L X, LEI F P. A new multiscale method of primary atomization[C]// Proceedings of The 5th CSA- IAA Conference on Advanced Space Technology. Shanghai, China: CSA-IAA, 2013: 21-23.
[31]VALLIER A, REVSTEDT J, NILSSON H. Procedure for the break-up of cavitation sheet[C]// Proceedings of 4th International Meeting on Cavitation and Dynamic Prob- lems in Hydraulic Machinery and Systems. Belgrade, Serbia: [s.n.], 2011: 77-85.
[32]LI X Y, ARIENTI M, MARIOS C S. Towards an efficient, high-fidelity methodology for liquid jet atomization com- putations, AIAA-2010-210[R]. USA: AIAA, 2010.
[33]LI X Y, MARIOS C S. Prediction of high density-ratio liquid jet atomization in crossflow using high fidelity simulations on HPC, AIAA-2012-0175[R]. USA: AIAA, 2012.

相似文献/References:

[1]崔明功,郭 然.环形引射器流场研究[J].火箭推进,2015,41(02):75.
　CUI Ming-gong,GUO Ran.Study on flow field of annular ejector[J].Journal of Rocket Propulsion,2015,41(01):75.
[2]南向军.带抑流楔升力前体设计初探[J].火箭推进,2014,40(01):50.
　NAN Xiang-jun.Design of lift-forebody with transverse flow restraining wedge[J].Journal of Rocket Propulsion,2014,40(01):50.
[3]王海韵,王长辉,范匆.结构参数设计对微喷管性能的影响[J].火箭推进,2017,43(05):14.
　WANG Haiyun,WANG Changhui,FAN Cong.Effects of structure parameter design onperformance of micro-nozzle[J].Journal of Rocket Propulsion,2017,43(01):14.
[4]赵 鼎,刘 琳,孙龙飞.钛合金夹层结构扩散钎焊工艺研究[J].火箭推进,2018,44(01):67.
　ZHAO Ding,LIU Lin,SUN Longfei.Study on diffusion brazing process for titanium alloy sandwich structure[J].Journal of Rocket Propulsion,2018,44(01):67.
[5]高兴峰,张建伟,孙 冰,等.推力室头部最优气膜参数研究[J].火箭推进,2018,44(02):10.
　GAO Xingfeng,ZHANG Jianwei,SUN Bing,et al.Study on optimal gas film parameters of near-injection region in thrust chamber[J].Journal of Rocket Propulsion,2018,44(01):10.
[6]徐鸿鹏,张志涛,唐斌运,等.发动机试验液氧贮箱放气系统动态特性研究[J].火箭推进,2018,44(05):71.
　XU Hongpeng,ZHANG Zhitao,TANG Binyun,et al.Study on dynamic characteristics of gas-exhaust-system for liquid oxygen tank used for liquid rocket engine ground test[J].Journal of Rocket Propulsion,2018,44(01):71.
[7]宋大亮,凌前程,章荣军.双组元离心式喷嘴外喷嘴流动数值模拟分析[J].火箭推进,2018,44(04):10.
　SONG Daliang,LING Qiancheng,ZHANG Rongjun.Numerical analysis on flow characteristics of outer nozzle of bipropellant pressure-swirl injector[J].Journal of Rocket Propulsion,2018,44(01):10.
[8]姜金朋,石竟成,苏立超,等.叶型尺寸比例变化对预测涡轮气动性能和气动力的影响[J].火箭推进,2018,44(06):29.
　JIANG Jinpeng,SHI Jingcheng,SU Lichao,et al.Effects of airfoil scaling on the predicted aerodynamic performance and forcing of turbine[J].Journal of Rocket Propulsion,2018,44(01):29.
[9]杨瑞康,张勤练,周 舟,等.推力室外壁机器人自适应焊接控制研究[J].火箭推进,2019,45(01):66.
　YANG Ruikang,ZHANG Qinlian,ZHOU Zhou,et al.Research on robot adaptive welding control of thrust chamber outer wall[J].Journal of Rocket Propulsion,2019,45(01):66.
[10]周璟莹,邹伟龙,黄立还.冲压发动机风洞引射器引射性能模拟[J].火箭推进,2019,45(02):53.
　ZHOU Jingying,ZOU Weilong,HUANG Lihuan.Simulation study on ejection performance of ramjet engine wind tunnel ejector[J].Journal of Rocket Propulsion,2019,45(01):53.

备注/Memo

收稿日期：2013-08-13；修回日期：2013-09-18 基金项目：国家重大基础研究项目（613193） 作者简介：刘昌波（1979—），男，博士研究生， 研究领域为液体火箭发动机设计

更新日期/Last Update: 1900-01-01