[1] 孙明波.超声速来流稳焰凹腔的流动及火焰稳定机制[D].长沙:国防科技大学,2008.
[2] Ben-YakarA,HansonRK.CavityFlame-HoldersforIgnitionandFlameStabilizationinScramjets:anOverview[J].JournalofPropulsionandPower,2001,17(4):869-878.
[3] 丁猛.基于凹腔的超声速燃烧火焰稳定技术研究[D].长沙:国防科技大学,2005.
[4] AggarwalSK.AReviewofSprayIgnitionPhenomena:PresentStatusandFutureResearch[J].ProgressinEnergyandCombustorScience,1998,24:565-600.
[5] 席文雄,王振国,李庆,等.超声速气流中煤油喷雾的热射流强迫点火[J].航空动力学报,2012,27(11):2436-2441.
[6] 席文雄,王振国,刘卫东,等.超燃冲压发动机点火方案对比试验研究[J].推进技术,2013,34(3):383-389.(XIWen-xiong,WANGZhen-guo,LIUFig.13Upstreampropagationofpremixflamealongwallboundary2134推进技术2016年Wei-dong,etal.ExperimentalComparisonontheSchemeofIgnitioninDual-ModeScramjet[J].JournalofPropulsionTechnology,2013,34(3):383-389.)
[7] 俞刚,李建国,赵震,等.超声速模型燃烧室中气化煤油喷注研究[J].推进技术,2005,26(2):97-100.(YUGang,LIJian-guo,ZHAOZhen,etal.InvestigationofVaporizedKeroseneInjectioninaSupersonicModelCombustor[J].JournalofPropulsionTechnology,2005,26(2):97-100.)
[8] TaichangZhang,JingWang,XuejunFan.CombustionofVaporizedKeroseneinSupersonicModelCombustorswithDislocatedDualCavities[J].JournalofPropulsionandPower,2014,30(5).
[9] ViacheslavAV,YuriiMS,CorinS.ReviewofFuelPre-InjectionStudiesinaHighSpeedAirflow[R].AIAA2006-1030.
[10] JeanPS,BernardP.HypervelocityFuel/AirMixinginaShcramjetInlet[J].JournalofPropulsionandPower,2004,20(2).
[11] KurdyumovV,Fernandez-TarrazoE,TruffautJM,etal.ExperimentalandNumericalStudyofPremixedFlameFlashback[J].ProceedingsoftheCombustionInstitute,2007,31(1):1275-1282.
[12] 乔英杰,毛荣海.贫油预混预蒸发燃烧室回火现象的大涡模拟[J].航空学报,2014,35(6).
[13] 张群,范玮,徐华胜,等.低排放航空燃气轮机燃烧技术[J].航空制造技术,2013,9.
[14] SislianJP,MartensRP,SchwartzentruberTE.NumericalSimulationofaRealShcramjetFlowfield[J].JournalofPropulsionandPower,2006,22(5).
[15] MathurT,GruberMR,JacksonK,etal.SupersonicCombustionExperimentswithaCavity-BasedFuelInjector[J].JournalofPropulsionandPower,2001,17(6):1305-1312.
[16] O’ByrneS.StotzI,NeelyAJ,etal.OHPLIFImagingofSupersonicCombustionUsingCavityInjection[R].AIAA2005-3357.
[17] ChoiJY,NohJ,ByunJR,etal.NumericalInvestigationofCombustion/Shock-TrainInteractionsinaDual-ModeScramjetEngine[R].AIAA2011-2395.
[18] Ming-BoSun,Xing-DaCui,Hong-BoWang,etal.FlameFlashbackinaSupersonicCombustorFueledbyEthylenewithCavityFlameholder[J].JournalofPropulsionandPower,2015,31(3):976-980.
[19] 钟文丽,席文雄,段立伟,等.超声速气流点火助燃用等离子体火炬的试验研究[J].推进技术,2015,36(10):1528-1532.(ZHONGWen-li,XIWen-xiong,DUANLi-wei,etal.ExperimentalInvestigationonPlasmaTorchforSupersonicFlowfieldIgnitionandCombustion[J].JournalofPropulsionTechnology,2015,36(10):1528-1532.)(编辑:朱立影)
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