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Flow Resistance Characteristics of Rotary Ribbed Channels


文档名:Flow Resistance Characteristics of Rotary Ribbed Channels
Abstract:Withthedevelopmentofaero-engines,theturbineinlettemperaturecontinuestorise.Inordertoensurethesafetyandreliabilityoftheturbineblades,coolingstructuresmustbesetinsideturbinebladestocoolthem.Heattransfercoefficientandflowresistancearethekeyparameterstomeasurethecoolingcharacteristicsofinternalcoolingstructures.Inthispaper,thecharacteristicsofflowresistanceinarotatingribbedchannelispresentednumericalsimulationunderdifferentribspacings,ribangles,andthermalboundaryconditions.Theresultsshowthat,separationandreattachmentoffluidbetweenribsisthekeyeffectofribspacingonflowresistance.Theflowresistanceissmallwhentheribspacingissmall,becauseit'sdifficultforthefluidtoformreattachmentbetweentheribs.Withtheincreaseofribspacing,thereattachmentphenomenonismoreobviousandtheflowresistanceincreasesaccordingly.Ingeneral,p:e=10channelhasthemaximumflowresistance.Secondaryflowcausedbytheribsisthekeyfactoraffectingtheflowresistancecharacteristicswithdifferentribangles.Thesecondaryflowinteractswiththemainflowandcausesflowlossthroughmixing,thusaffectingtheflowresistanceofthechannel.Understaticcondition,theflowresistanceof60°ribbedchannelisthelargest.Theflowresistanceofchannelwasaffectedbythetemperatureriseratioalso.AndwiththeincreaseoftheRo,thetemperatureriseratiohasamoreobviouseffectontheflowresistanceoftheribbedchannel.WhenRo=0.45,theflowresistanceofthechannelwithatemperatureriseratioof0.4is2.4timesthatofthechannelwithouttemperaturerise,whilewhenRo=0.3,itis1.6times,andwhenRo=0.15,itis1.2times.

作者:Ru-quanYou   Yun-tengXu   Hai-wangLi Author:Ru-quanYou   Yun-tengXu   Hai-wangLi
作者单位:NationalKeyLaboratoryofScienceandTechnologyonAeroEnginesAero-thermodynamics,BeihangUniversity;ResearchInstituteofAero-Engine,BeihangUniversity;AdvancedJetPropulsionInnovationCenter,AEAC;TianmushanLaboratoryNationalKeyLaboratoryofScienceandTechnologyonAeroEnginesAero-thermodynamics,BeihangUniversity;ResearchInstituteofAero-Engine,BeihangUniversityNationalKeyLaboratoryofScienceandTechnologyonAeroEnginesAero-thermodynamics,BeihangUniversity;ResearchInstituteofAero-Engine,BeihangUniversity;TianmushanLaboratory
刊名:风机技术
Journal:Compressor,Blower&FanTechnology
年,卷(期):2024, 66(2)
分类号:
Keywords:BladeCoolingRibbedPassageRotationFlowResistanceCharacteristics
机标分类号:SO241.3P228.4
在线出版日期:2024年5月21日
基金项目:FlowResistanceCharacteristicsofRotaryRibbedChannels[
期刊论文]风机技术--2024, 66(2)Ru-quanYouYun-tengXuHai-wangLiWiththedevelopmentofaero-engines,theturbineinlettemperaturecontinuestorise.Inordertoensurethesafetyandreliabilityoftheturbineblades,coolingstructuresmustbesetinsideturbinebl...参考文献和引证文献
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