Shockwave/turbulentboundarylayerinteractions(STBLIs)commonlyoccurintheinternalorexternalflowofsupersonicorhypersonicvehiclesandhaveanimportantinfluenceonaerodynamiccharacteristics.WalltemperaturehasbecomearesearchemphasisbecauseofitssignificanteffectsoncompressibleboundarylayersandSTBLIs.Recently,theresearchteamledbyProf.LiXinliangfromtheInstituteofMechanics,ChineseAcademyofSciences,conducteddirectnumericalsimulations(DNSs)toinvestigatethewalltemperatureeffectsonhypersonicSTBLIs.Thisresearchfocusedonelucidatingthemechanismsofwalltemperatureeffectsontheflowstructuresandlow-frequencyunsteadiness,andderivedanequationtopredictthewallpressuredistributionatdifferentwalltemperatures.Thework,titled"Effectsofwalltemperatureonhypersonicshockwave/turbulentboundarylayerinteractions,"hasbeenpublishedintheJournalofFluidMechanics,withauthorsincludingZhangJi,GuoTongbiao,DangGuanlin,andLiXinliang.Inthisresearch,theheterogeneousparallelfinitedifferencesolverOpenCFD-SCUisadoptedfortheDNSsofSTBLIsovera34°compressionrampatMachnumber6.Threevaluesofthewall-to-recovery-temperatureratio(0.50,0.75,and1.0)areconsideredinthesimulations.Figure1showsanumericalresult(Iso-surfacesofQwiththeadiabaticwall)withhighspatiotemporalresolution.Theresearchindicatesthatcoolingthewallcanreducethesizeoftheseparationbubble,asshowninfigure2.Thisisbecauseacolderwallcontributestofullerprofilesofdensityandvelocityintheturbulentboundarylayer,leadingtoagreatermomentumofthenear-wallfluidtoresisttheseparation.Figure1.Iso-surfacesofinstantaneousQ=0.1colouredbythestreamwisevelocityinthecasesof.Figure2.Contoursofthemeanstreamwisevelocityandstreamlinesinthex-yplaneinthecasesof(a),(b),and(c).AccordingtotheFITandthesimulationdata,thefollowingequationisproposedtodescribethewallpressureriseprocessupstreamfromthecornerwhenthewalltemperaturechanges:whereniscloseto0.85inthecompressionrampSTBLIs.Figure3showsthattheresultspredictedbythisequationaregenerallyconsistentwiththoseofthesimulations.Figure3.Predictionresultsofthemeanwallpressureat(a)M∞=2.9and(b)M∞=6.0.Theanalysisbasedontheweightedpowerspectraldensity(WPSD)indicatesthatcoolingthewallcansignificantlysuppressthelow-frequencyunsteadinessbyreducingtheenergyofthelow-frequencymotionandnarrowingitsstreamwiserange,asshowninfigure4.Theanalysisofthecorrelationbetweentheupstreamanddownstreamflowsindicatesthatthelow-frequencyunsteadinessismainlydrivenbythedownstreammechanism.Therefore,thesuppressedlow-frequencyunsteadinessiscausedbythedecreasingsizeoftheseparationbubblewhenthewalltemperaturedecreases.Figure4.ContoursofthewallpressureWPSDinthecasesof(a),(b),and(c).Linktothepaper:https://doi.org/10.1017/jfm.2024.533
Prof . ZHANG Jin and A . P . JIAN Muqiang from Peking University and the Beijing Graphene Institute , Prof . WU Xianqian from the Institute of Mechanics , Chinese Academy of Sciences , P . GAO Enlai from Wuhan University .Chinese Academy of Sciences and their teams ? developed a strategy to fabricate carbon nanotube fibers with the dynamic strength up to 14 GPa . This work has been published in Science with the title of “ Carbon nanotube fibers with dynamic strength up to 14 GPa . ” on June.
The edge crack problem is often observed in engineering applications. It is one of the most prominent factors causing damage and failure of engineering structures, and it is also one of the classical problems in fracture mechanics. Due to the structure heterigenety and the loading conditions complexity, multiple cracks often occur on the edge. The interaction between cracks will affect the crack propagation path and the failure mode of the structure. To study the mechanical properties of multiple edge cracks under different loading conditions is of great engineering significance. Engineers can rationally use the interaction between cracks to improve the life of structures under specific working conditions.
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