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低雷诺数下旋转圆柱升力系数数值计算分析 Title:NumericalanalysisoftheLiftCoefficientforarotatingcylinderatlowReynoldsnumbers Abstract: TheliftcoefficientisacrucialparameterinunderstandingtheaerodynamicperformanceofarotatingcylinderatlowReynoldsnumbers.Inthisstudy,anumericalanalysisisconductedtoinvestigatetheliftcoefficientforarotatingcylinderanditsdependenceonvariousfactorssuchasrotationalspeedandReynoldsnumber.Thecomputationalfluiddynamics(CFD)techniqueisemployedtosimulatetheflowfieldaroundthecylinderandcalculatetheliftcoefficient.TheresultsdemonstratethesignificanceofReynoldsnumberindeterminingtheliftcoefficientandprovidevaluableinsightsintotheaerodynamiccharacteristicsofrotatingcylindersatlowReynoldsnumbers. 1.Introduction: Rotatingcylindersarewidelyencounteredinengineeringapplications,rangingfromhelicopterrotorstowindturbineblades.Understandingtheaerodynamicperformanceofrotatingcylindersiscrucialforoptimizingtheirdesignandensuringefficientoperation.Theliftcoefficient,whichquantifiestheliftforcegeneratedbythecylinder,playsavitalroleindeterminingitsaerodynamicefficiency.AtlowReynoldsnumbers,theflowcharacteristicsaroundrotatingcylindersdiffersignificantlyfromthoseathigherReynoldsnumbers,makingtheanalysisofliftcoefficientsmorechallengingandintriguing. 2.Literaturereview: PreviousstudieshaveinvestigatedtheliftcoefficientofrotatingcylindersatdifferentReynoldsnumbers.SumerandFredsoe(1997)conductedexperimentalinvestigationsusingphysicalmodelstoobservetheeffectofrotationalspeedandReynoldsnumberontheliftcoefficient.Theyfoundasignificantincreaseintheliftcoefficientwithanincreaseinrotationalspeed,whiletheeffectofReynoldsnumberwaslesspronounced.Ontheotherhand,Zhouetal.(2001)employedcomputationalsimulationstoexploretheflowfieldaroundrotatingcylindersatlowReynoldsnumbers.TheirresultsindicatedthattheliftcoefficientdependsstronglyonReynoldsnumber. 3.Methodology: Inthisstudy,anumericalapproachutilizingcomputationalfluiddynamics(CFD)isappliedtosimulatetheflowaroundarotatingcylinderatlowReynoldsnumbers

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