[1] CharlesR,McClinton.X-43-ScramjetPowerBreakstheHypersonicBarrierDrydenLectureshipinResearchfor2006[R].AIAA2006-1880.
[2] TakahashiS,DemiseS,OshitaM.CorrelationBetweenHeatFluxDistributionandCombustionModeinaScramjetCombustor[R].AIAA2001-1191.
[3] LeDB,GoyneCP,KraussRH.ExperimentalStudyofaDual-ModeScramjetIsolator[J].JournalofPropulsionandPower,2008,24(5):1050-1057.
[4] FotiaML,DriscollJF.IsolatorCombustorInteractionsinaDirect-ConnectRamjet-ScramjetExperiment[J].JournalofPropulsionandPower,2012,28(1):83-95.
[5] MatthewLFotia,JamesFDriscoll.Ram-ScramTransitionandFlame/Shock-TrainInteractionsinaModelScramjetExperiment[J].JournalofPropulsionandPower,2013,29(1):261-273.
[6] MatthewLFotia,JamesFDriscolly.ExperimentalInvestigationofRam/Scram-ModeTransitionMechanics[R].AIAA2012-5835.
[7] EdwardTC.ScramjetEngines:theFirstFortyYears[J].JournalofPropulsionandPower,2001,17(6):1138-1148.
[8] MitaniT,ChinzeiN,KandaT.ReactionandMixing-ControlledCombustioninScramjetEngines[J].JournalofPropulsionandPower,2001,17(2):308-314.
[9] SadatakeTomioka,AtsuoMurakami,KenjiKudo,etal.CombustionTestsofaStagedSupersonicCombustorwithaStrut[J].JournalofPropulsionandPower,2001,17(2):293-300.
[10] KanKobayashi,SadatakeTomioka,KanenoriKato,etal.PerformanceofaDual-ModeCombustorwithMultistagedFuelInjection[J].JournalofPropulsionandPower,2006,22(3):518-526.
[11] TakeshiKanda,NobuoChinzei,KenjiKudo,etal.Dual-ModeOperationsinaScramjetCombustor[J].JournalofPropulsionandPower,2004,20(4):760-763.
[12] KanenoriKato,TakeshiKanda,KanKobayashi,etal.DownstreamRamjet-ModeCombustioninaDual-ModeScramjetEngine[J].JournalofPropulsionandPower,2006,22(3):511-517.
[13] 李大鹏.煤油双模态冲压发动机燃烧室工作过程研究[D].长沙:国防科学技术大学,2006.
[14] 陈强,陈立红,顾洪斌,等.释热分布对超燃冲压发动机性能的影响及优化[J].推进技术,2009,30(2):135-138.(CHENQiang,CHENLI-hong,GUHong-bin,etal.InvestigationoftheEffectandOptimizationofHeatReleaseDistributionsintheCombustoronScramjetPerformance[J].JournalofPropulsionTechnology,2009,30(2):135-138.)
[15] 姚照辉,李光熙,张蒙正,等.燃油分配对超燃冲压2022推进技术2016年发动机的性能影响仿真分析[J].火箭推进,2013,39(4):30-35.
[16] 肖保国,晏至辉,田野,等.超燃发动机燃烧模态判别准则初步研究[J].推进技术,2015,36(8):1121-1126.(XIAOBao-guo,YANZhi-hui,TIANYe,etal.PreliminaryStudyonDistinguishCriterionofCombustionModeforScramjet[J].JournalofPropulsionTechnology,2015,36(8):1121-1126.)
[17] 王西耀,肖保国,田野,等.当量比对燃烧模态的影响机理分析[J].推进技术,2015,36(4):488-494.(WANGXi-yao,XIAOBao-guo,TIANYe,etal.TheAnalysisofInfluenceofFuel-AirRatioontheMechanismofCombustionMode[J].JournalofPropulsionTechnology,2015,36(4):488-494.)
[18] ShunhuaYang,JialingLe.ComputationalAnalysisofaKerosene-FueledScramjet[R].ISABE-2005-1195.
[19] 肖保国,杨顺华,邢建文,等.并行原位自适应建表方法在超燃计算中的应用[J].推进技术,2010,31(4):412-417.(XIAOBao-guo,YANGShun-hua,XINGJian-wen,etal.AnApplicationofParallelinsituAdaptiveTabulationMethodinCalculationofSupersonicCombustion[J].JournalofPropulsionTechnology,2010,31(4):412-417.)
[20] 肖保国.碳氢燃料简化动力学模型和当地自适应建表方法在超燃并行计算中的应用[D].绵阳:中国空气动力研究与发展中心,2009.
[21] DanielJMicka,SeanMTorrez,JamesFDriscoll.HeatReleaseDistributioninaDual-ModeScramjetCombustor-MeasurementsandModeling[R].AIAA2009-7362.(编辑:梅瑛)
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