亚声速横向气流中液体射流破碎过程的直接模拟

推进技术 ›› 2016, Vol. 37 ›› Issue (11): 2135-2141.

亚声速横向气流中液体射流破碎过程的直接模拟

刘日超^1,2,乐嘉陵²,杨顺华²,郑忠华²,宋文艳¹,黄渊²

西北工业大学动力与能源学院，陕西西安710072;中国空气动力研究与发展中心超高速空气动力研究所高超声速冲压发动机技术重点实验室，四川绵阳621000,中国空气动力研究与发展中心超高速空气动力研究所高超声速冲压发动机技术重点实验室，四川绵阳621000,中国空气动力研究与发展中心超高速空气动力研究所高超声速冲压发动机技术重点实验室，四川绵阳621000,中国空气动力研究与发展中心超高速空气动力研究所高超声速冲压发动机技术重点实验室，四川绵阳621000,西北工业大学动力与能源学院，陕西西安710072,中国空气动力研究与发展中心超高速空气动力研究所高超声速冲压发动机技术重点实验室，四川绵阳621000

发布日期:2021-08-15
作者简介:刘日超，男，博士生，研究领域为燃烧室燃烧与流动。

DirectNumericalSimulationsofAtomizationProcesses

SchoolofPowerandEnergy，NorthwesternPolytecnicalUniversity，Xi’an710072，China;ScienceandTechnologyonScramjetLaboratory，HypervelocityAerodynamicsInstitute， CARDC，Mianyang621000，China,ScienceandTechnologyonScramjetLaboratory，HypervelocityAerodynamicsInstitute， CARDC，Mianyang621000，China,ScienceandTechnologyonScramjetLaboratory，HypervelocityAerodynamicsInstitute， CARDC，Mianyang621000，China,ScienceandTechnologyonScramjetLaboratory，HypervelocityAerodynamicsInstitute， CARDC，Mianyang621000，China,SchoolofPowerandEnergy，NorthwesternPolytecnicalUniversity，Xi’an710072，China and ScienceandTechnologyonScramjetLaboratory，HypervelocityAerodynamicsInstitute， CARDC，Mianyang621000，China

Published:2021-08-15

摘要/Abstract

摘要： 为研究亚声速横向气流中液体射流柱的变形、弯曲以及其破碎过程，利用LES结合VOF的

关键词: RT不稳定性；射流柱；首次破碎；雾化

Abstract: Inordertodeeplyresearchthemechanismsofcolumndistortion，bendandbreakingupwhena

Key words: Rayleigh-Taylor(RT)instability；Spraycolumn；Primarybreakup;Atomization

刘日超,乐嘉陵,杨顺华,郑忠华,宋文艳,黄渊. 亚声速横向气流中液体射流破碎过程的直接模拟[J]. 推进技术, 2016, 37(11): 2135-2141.

LIURi-chao^1,2,LEJia-ling²,YANGShun-hua²,ZHENGZhong-hua²,SONGWen-yan¹,HUANGYuan². DirectNumericalSimulationsofAtomizationProcesses[J]. Journal of Propulsion Technology, 2016, 37(11): 2135-2141.

[1] BusquinP,ArguellesP.EuropeanAeronautics:AVisionfor2020-ASynopsis[R].Air&SpaceEuropean,2001,3(s3-4):16-18.
[2] Pei-KuanWu,KevinA.BreakupProcessesofLiquidJetsinSubsonicCrossflows[R].AIAA96-3024.
[3] PrakashRSurya,HrishikeshGadgil.BreakupProcessesofPressureSwirlSprayinGaseousCross-Flow[J].InternationalJournalofMultiphaseFlow,2014,66(7):(a)(b)Fig.9Velocitycontourbesideofspray(a)Spraycolumn(b)Z=0Fig.10Spraycolumn(Vl=22m/s,Va=21m/s)(a)Spraycolumn(b)Z=0Fig.11Spraycolumn(Vl=22m/s,Va=60m/s)第37卷第11期亚声速横向气流中液体射流破碎过程的直接模拟214179-91.
[4] MazallonJ,DaiZ.AerodynamicPrimaryBreakupattheSurfaceofNonturbulentRoundLiquidJetsinCrossflow[R].AIAA1998-716.
[5] 朱英,黄勇.横向气流中的液体圆形射流破碎实验[J].航空动力学报,2010,25(10):2216-2266.
[6] 孙慧娟,刘利.横流中喷雾掺混流场结构研究[J].推进技术,2012,33(2):221-226.(SUNHui-juan,LIULi.InvestigationofMixingFlowFieldofSprayDropletsinCrossflow[J].JournalofPropulsionTechnology,2012,33(2):221-226.)
[7] HaibinZhang,BofengBai.ExperimentalStudyoftheMixingofTwoImpingingPressure-SwirlSpraysinCrossflow[J].ExperimentalThermalandFluidScience,2013,49(9):67-74.
[8] HaibinZhang,BofengBai.DropletDispersionCharacteristicsoftheHollowConeSpraysinCrossflow[J].ExperimentalThermalandFluidScience,2013,45(2):25-33.
[9] 刘静,徐旭.高速气流中横向液体射流雾化研究进展[J].力学进展,2009,39(3):273-283.
[10] 林宇震,李林.液体射流喷入横向气流混合特性研究进展[J].航空学报,2014,35(1):46-57.
[11] 郭婷婷,李少华.横向紊动射流的数值与实验研究进展[J].力学进展,2005,35(2):211-220.
[12] AlirezaMashayek.ExperimentalandNumericalStudyofLiquidJetsinCrossflows[D].Toronto:UniversityofToronto,2006.
[13] LiuFSmallwood.NumericalStudyofBreakupProcessesofWaterJetInjectedintoaCrossAirFlow[C].USA:ICLASS2000ProceedingsoftheEighthInternationalConferenceonLiquidAtomizationandSpraySystems:67-74.
[14] KuoKK.RecentAdvancesinSprayCombustion:SprayAtomizationandDropBurningPhenomena[R].AIAA96-866418.
[15] SinaGhods.DetailedNumericalSimulationofLiquidJetinCrossflowAtomizationwithHighDensityRatios[D].USA:ArizonaStateUniversity,2013.
[16] HirtCW,NicholsBD.VolumeofFluid(VOF)MethodfortheDynamicsofFreeBoundaries[J].JournalofComputationalPhysics,1981,39(81):201-225.
[17] YoungsDL.Time-DependentMulti-MaterialFlowwithLargeFluidDistortion[M].Aldermaston:AtomicWeaponsResearchEstablishment,1982.
[18] UbbinkO.NumericalPredictionofTwoFluidSystemswithSharpInterfaces[D].London:ImperialCollegeofScience,TechnologyandMedicine,1997.
[19] Chee-LoonNG.Deformation,WavePhenomena,andBreakupOutcomesofRoundNonturbulentLiquidJetsinUniformGaseousCrossflow[D].USA:OklahomaStateUniversity,2006.
[20] MartinezJM,ChensneauX,ZeghmatiB.ANewCurvatureTechniqueCalculationforSurfaceTensionContributioninPLIC-VOFMethod[J].ComputationalMechanics,2006,37(2):182-193.
[21] DexjardinsO,MoureauV,PitschH.AnAccurateConservativeLevelSet/GhostFluidMethodforSimulatingTurbulentAtomization[J].JournalofComputationalPhysics,2008,227(18):8395-8416.
[22] ShinjoJ,UmemuraA.SimulationofLiquidJetPrimaryBreakup:DynamicsofLigamentandDropletFormation[J].InternationalJournalofMultiphaseFlow,2010,3(8):513-532.
[23] 刘娟,李清廉,刘卫东.离心式喷嘴液膜破碎过程实验[J].推进技术,2011,32(4):539-543.(LIUJuan,LIQing-lian,LIUWei-dong.ExperimentonLiquidSheetBreakupProcessofPressureSwirlInjector[J].JournalofPropulsionTechnology,2011,32(4):539-543.
[24] 刘儒勋,刘晓平,张磊.运动界面的追踪和重构方法[J].应用数学和力学,2004,25(3):279-290.
[25] 刘日超,乐嘉陵.直流喷射首次破碎的形变过程研究[J].推进技术,2016,37(7).(LIURi-chao,LEJialing.InvestigationofDeformationofPrimaryBreakupinDirectInject[J].JournalofPropulsionTechnology,2016,37(7).)(编辑:梅瑛)