简介：NumericaltechniquesplayanimportantroleinCFD.Someofthemarereviewedinthispaper.ThenecessityofusinghighorderdifferenceschemeisdemonstratedforthestudyofhighReynoldsnumberviscousflow.Physicalguidelinesareprovidedfortheconstructionofthesehighorderschemes.Toavoidundulyadhoctreatmentintheboundaryregiontheuseofcompactschemeisrecommendedbecauseithasasmallstencilsizecomparedwiththetraditionalfinitedifferencescheme,BesidespreliminaryFourieranalysisshowsthecompactschemecanalsoyieldbetterspaceresolutionwhichmakesitmoresuitabletostudyflowwithmultiscalese.g.turbulence.Otherapproachessuchasperturbationmethodandfinitespectralmethodarealsoemphasized.Typicalnumericalsimulationswerecarriedout.ThefirstdealswithEulerequationstoshowitscapabilitiestocaptureflowdiscontinuity.TheseconddealswithNavier-Stokesequationsstudyingtheevolutionofamixinglayer,thepertinentstructuresatdifferenttimesareshown.Asymmetricbreakdownoccursandalsotheappearanceofsmallvortices.

简介：Thispaperdevelopsahypersonicaerothermalsimulationmethodformissileslotflow.ThefinitevolumemethodofstructuregridsolverisdevelopedforsolvingEulerandNavier-Stokesequations.ThesolverincludesPark'stwotemperaturemodelandtheairmulti-speciesreactionmodel.Thesecond-orderaccuracyTVDnumericalmethodwasdeducedtocomputethehypersonicaeroheatingwhichimprovesthecomputationalefficiency.Computationalresultsaregiventoshowthehighaccuracycomparingtotheexistingexperimentaldata.

简介：NowadaysComputationalFluidDynamics(CFD)softwareisadoptedasadesignandanalysistoolinagreatnumberofengineeringfields.Wecansaythatsingle-physicsCFDhasbeensufficientlymaturedinthepracticalpointofview.ThemaintargetofexistingCFDsoftwareissingle-phaseflowssuchaswaterandair.However,manymulti-physicsproblemsexistinengineering.Mostofthemconsistofflowandotherphysics,andtheinteractionsbetweendifferentphysicsareveryimportant.Obviously,multi-physicsphenomenaarecriticalindevelopingmachinesandprocesses.Amulti-physicsphenomenonseemstobeverycomplex,anditissodifficulttobepredictedbyaddingotherphysicstoflowphenomenon.Therefore,multi-physicsCFDtechniquesarestillunderresearchanddevelopment.Thiswouldbecausedfromthefactsthatprocessingspeedofcurrentcomputersisnotfastenoughforconductingamulti-physicssimulation,andfurthermorephysicalmodelsexceptforflowphysicshavenotbeensuitablyestablished.Therefore,innearfuture,wehavetodevelopvariousphysicalmodelsandefficientCFDtechniques,inordertosuccessmulti-physicssimulationsinengineering.Inthepresentpaper,Iwilldescribethepresentstatesofmulti-physicsCFDsimulations,andthenshowsomenumericalresultssuchasiceaccretionandelectro-chemicalmachiningprocessofathree-dimensionalcompressorbladewhichwereobtainedinmylaboratory.Multi-physicsCFDsimulationswouldbeakeytechnologyinnearfuture.

简介：Acombustionmodelofalarge-scalesupercriticalcirculatingfluidizedbed(CFB)boilerwasdevelopedforcomprehensivecomputational-fluid-dynamicsanalysis.Themodelincorporatesgas-solidhydrodynamics,coalcombustion,heattransferonheatexchangesurfacesinthefurnace,andheattransferbetweenfumaceandworkingmediumintheheattransfertubes.Insimulatingthedenseanddilutephasesinthefumace,thegas-solidhydrodynamicsisbasedontheEuler-Eulermodelandenergy-minimizationmultiscaledragmodel.Coalcombustionentailsevaporation,devolatilization,charcombustion,gashomogeneousreaction,andpollutantemission.Thecoefficientofheattransferbetweengas-solidandthewaterwallisestimatedusingtheclusterrenewalmodel,andforradiation,thediscreteordinatemodelisused.Moreover,thermohydraulicprocessesinthemembranewallarealsoineludedintheheattransferprocess.Themodelwassuccessfullyappliedinsimulationsofa350-MWsupercriticalCFBboiler.Detaileddistributionsofsolidsconcentration,oxygen,heatflux,andworkingmediumtemperatureintheboilerfurnacearepresented.

简介：Gas-solidtwo-phaseflowinacirculatingfluidizedbed(CFB)isaffectedbyoperatingconditions(e.g.,superficialgasvelocity,solidsinventory),materialpropertiesandgeometricfactors,suchastheentryandexitconfiguration.Inparticular,thesuspensionsection,whichislocatedbetweentheriserbottomandthesolidsrecycleinlet,affectsthehydrodynamicsintherisersignificantly.However,thesuspensionsectionhasreceivedlessattentioncomparedwithothergeometricfactors.Mostcomputationalfluiddynamics(CFD)simulations,especiallytwo-dimensionalsimulationsdonottakethisfactorintoaccount.Weperformedthree-dimensional,full-loopCFDsimulationswithadragcoefficientthatwasdeterminedbytheenergy-minimizationmulti-scalemodel,andinvestigatedtheflowbehavioroftwoCFBswithdifferentsuspension-sectionlengths.ThesimulationresuitsrevealedthattheaxialprofilesofvoidageintheriserwithalongersuspensionsectionaremorelikelyS-shaped,whereasthosewithshortersuspensionsectionsdecayexponentially.ThedependencesofsolidsfluxonsolidsinventorydifferinthetwoCFBs.Ashortersuspensionsectionmayresultinasmoothtransitionfromdilutetodensetransportwithoutintermediateaccumulativechoki-ng,whereasaIongersuspensionsectionmayleadtoachokingtransition.Thesesimulationresultsarequalitativelyconsistentwiththeflowbehaviorsdescribedinliterature.

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简介：Inaclassicallayoutprocessofafanthequantityoflossesisestimatedasasumandexpressedintheoverallefficiencyrateη.Howeverthecharacteristicofthepressurerise,thelossesandtheefficiencyratebesidethedesignpointisnotknown.Againstthisbackgroundanumericalmodelwasdevelopedtocalculatequantitativevaluesofoccurringlossesatradialfanimpellersatanearlystageinthedesignprocess.Itallowstoestimatethepressureriseandefficiencyrateofagivenfangeometryatandbesidethedesignpoint.Thephysicsoflossesaredescribedinliterature,butobtainingquantitativevaluesisstillachallenge.Ascommoninhydraulictheorythelossesarecalculatedwithanalyticformulassupportedbycoefficientsandefficiencyrates,whichhavetobedeterminedempirically.Thispapershowsthemethodhowtodeterminethecoefficientsforagivenradialfan.Thereforearepresentativeradialfanwithbackwardcurvedbladeswasdesignedinreferencetoclassicaldesignguidelines.PerformancemeasuringwasdoneconformtoISO5801.Theflowwascalculatedat8differentoperationpointsusingCFDmethods.TheRANSequationsaresolvedbyusingtheSST-k-omegaturbulencemodel.Theflowdomainconsistsofonebladesectionincludinginletchannelandoutflowchamber.Spatialdiscretizationisdonebyablock-structuredmeshofapprox.1.8millioncells.Performancedatashowaverygoodagreementbetweenmeasurementandcalculation.

简介：ControllingthesizeoffragraneemicrocapsulesusingdesignedagitatorpaddleswasinvestigatedandstudiedbyCFDsimulation.First,differentfluidflowswereestablishedbyvaryingstirringspeeds,reactorscales,andagitatorpaddledesign,andtheeffectsofeachonparticlesizeanddistributionofpreparedmicrocapsulesweredetermined.Theexperimentalresultsshowedthatthepatterndesignoforificesintheplatepaddlescontroltheflowfieldwell.Narrowparticle-sizedistributionsofthemicrocapsuleswereobtained.Thefluidflowcharacteristicsincludingfluidvelocityfield,turbulentkineticenergyfield,andshearstressdistributionforthedifferentagitatorpaddletypesindifferentreactionkettlesweresimulatedusingCFDtechnology.Thecorrelationsbetweensimulateddataandexperimentalresultswereanalyzed.Significantly,thesimulatedaverageflowvelocitywasfoundtoshowgoodnegativelinearcorrelationw让htheaverageparticlesizeofpreparedmicrocapsules,withacorrelationofy=-2.166x+42.626.

简介：在传播的Gassolid流动使流体化床(CFB)起床人操作条件取决于不仅而且在出口配置上。很少研究用计算液体动力学(CFD)在流动结构上调查了出口配置的效果。这份报纸提供2D与光滑、T突然的出口模仿一个冷凳子规模平方剖面图起床人的二液体的模型。在煤气、稳固的阶段之间的drag力量在CFD起一个重要作用。因为drag力量模型例如Wen-Yu关联，不能在gassolid流动基于同类的二阶段的流动捕获异构的结构，结构依赖者精力最小化多尺度(扩展内存管理程序)拖力量模型(王，Ge，与李，2008)，为GeldartB粒子(沙)适用，集成于二液体的模型。计算轴的固体停顿侧面为T突然的出口是为光滑的出口和塑造C的曲线的分别地指数的曲线，与试验性的数据一致的两个。这研究再次证明关键角色在CFD模拟并且也拖力量显示CFD模拟(二液体的模型)的有效性在CFB起床人在gassolid流动上描述出口效果。

简介：一条多维的计算液体动力学(CFD)途径在试图计算一台引擎的转移矩阵的这研究被建议有或没有吝啬的流动处于条件用尽muffler。没有吝啬的流动，有定义为多孔的地区的吸收性的材料的muffler的CFD模型与测量噪音减小被校准，并且进一步被采用在muffler的声学的表演上学习吝啬的流动的效果。而且，exhaust听觉的来源从建议CFD途径以及测量尾巴噪音最不基于multiload获得的六不同另外的声学的负担的计算转移矩阵被导出广场方法。最后，exhaust噪音基于Thevenins定理被预言。建议CFD途径被建议能就吝啬的流动而言预言复杂muffler的声学的表演(没有并且与吝啬的流动)并且加热转移，并且提供exhaust噪音的合理结果。

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简介：计算液体动力学(CFD)广泛地被用来学习gassolid使液化的水动力学；然而，它在liquidsolid使液化的应用是相对稀罕的。在这研究，liquidsolid的CFD模拟使流体化床被执行，集中于效果在liquidsolid使液化的水动力学上拖关联和增加的集体力量。拖关联，这被显示出模拟结果和关联上的重要效果由Beetstra等求婚了。(2007)与试验性的数据给最好的协议。我们进一步证明增加的集体力量确实在liquidsolid使液化的CFD模拟起一个重要作用，不应该因此在CFD模拟被忽略。

简介：Meso-scalestructuresexistingintheformofparticle-richclusters,streamersorstrandsincirculatingfluidizedbeds,andofascendingbubbleplumesanddescendingliquid-richvorticesinbubblecolumnsandslurry-bedreactors,ascommonlyobserved,haveplayedanimportantroleinthemacro-scalebehaviorofparticle-fluidsystems.Thesemeso-scalestructuresspanawiderangeoflengthandtimescales,andtheirorigin,evolutionandinfluencearestillfarfrombeingwellunderstood.Recentdecadeshavewitnessedtheemergenceofcomputersimulationofparticle-fluidsystemsbasedoncomputa-ionalfluiddynamic(CFD)models.However,strictlyspeakingthesemodelsarefarfrommatureandthecomplexnatureofparticle-fluidsystemsarisingfromthemeso-scalestructureshasbeenposinggreatchallengestoinvestigators.Thereasonmaybethatthecurrenttwo-fluidmodels(TFM)arederivedeitherfromcontinuummechanicsbyusingdifferentkindsofaveragingtechniquesfortheconservationequationsofsingle-phaseflow,orfromthekinetictheoryofgasesinwhichtheassumptionofmolecularchaosisemployed,therebylosingsightofthemeso-scaleheterogeneityatthescaleofcomputationalcellsandleadingtoinaccuratecalculationoftheinteractionforcebetweenparticlesandfluids.Forexample,theoveralldragforceforparticlesinacellisusuallycalculatedfromtheempiricalWen&Yu/Erguncorrelations,whichshouldbesuspectedsincethesecorrelationswereoriginallyderivedfromhomogeneoussystems.Schemestosolvethisproblemforgas-particlessystemsmaybeclassifiedintofourcategories.First,onecouldcapturethedetailedmeso-scalestructureinformationatthecellscalebyemployingtheso-calleddirectnumericalsimulation(DNS)(Hu,1996),thepseudo-particlemodeling(PPM)(Ge&Li,2003),ortheLattice-Boltzmannmethod(LBM)totracktheinterfacebetweengasandparticles.Second,refinementofthecomputationalmeshesmayreducetheheterogeneitytosomeextentandmaybe

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简介：文章以飞行器巡航外形为设计对象，构建了一种新的飞行器的气动和结构特性评估方法，即结构模型反迭代方法．该方法较传统的松耦合静气动弹性方法效率提高了4倍以上．以此为基础建立了一种新的飞行器气动／结构耦合多学科优化设计框架，将优化效率提高4倍以上．采用数值求解N—S方程和结构有限元方程方法作为气动和结构学科的分析工具，保证了设计结果的可信性．算例表明以巡航外形作为设计对象能够获得与传统方法一致的飞行器气动与结构特性，以此为基础开展的无人机气动外形优化设计也获得了良好的设计结果．

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简介：在动态网格上通过耦合求解流动控制方程和结构动力学方程,发展了一种舵面控制下飞行器运动响应过程中气动弹性数值模拟研究方法.流动控制方程采用N-S方程,结构动力学采用线性模态叠加方法,其中流动控制方程空间离散采用基于非结构网格的有限体积方法,对流通量采用计算HLLC格式,非定常时间离散采用基于LU-SGS的双时间步长方法.模拟中,气动运动和结构变形在双时间步长方法推进过程中采用改进松耦合方法,气动网格与结构网格之间信息交换采用无限平板样条法实现,飞行器的运动和变形采用基于重叠网格和Delaunay图映射变形网格相结合的方法进行处理.采用多个考核算例对发展的数值方法进行考核验证,结果表明该方法可以高效精确模拟舵面开环控制下飞行器运动响应过程中的气动弹性特性.

简介：为研究子母弹在抛撒时的干扰流场特性,选取多舱段子母弹为计算模型,基于课题组自主开发的非结构混合网格Reynolds平均Navier-Stokes方程求解程序HUNS3D,结合非结构嵌套网格技术,耦合六自由度刚体运动学方程,使用了改进的4阶Adams预估-校正法求解六自由度刚体运动方程.利用跨声速下典型外挂物分离作为验证算例,仿真结果与实验结果高度拟合,验证了求解器的精度.对锁定母弹自由度和释放母弹的自由度两种计算状态进行数值模拟.仿真结果表明:由于激波干涉作用,子弹与母弹之间有较强的耦合作用;释放母弹自由度后,子弹的气动力参数发生了较大变化.

简介：反推力装置能显著减小现代涡轮风扇支线飞机的着陆滑跑距离，也会影响到飞机的操稳特性和发动机进口流场特性，如果不能很好地和飞机进行匹配设计，则可能危及飞行安全．文章对某型尾吊布局民机全机着陆叶栅式反推力装置打开构型进行了CFD数值模拟，并对发动机反推装置打开与全机的匹配问题进行了评估，结果显示，Mach数0．09可作为该型民机反推装置安全使用的截止速度．