[1] DollingDS.FiftyYearsofShockWave/BoundaryLayerInteractionResearch:WhatNext?[J].AIAAJournal,2001,39(8):1517-1531.
[2] 宋文艳,马晓锋,刘伟雄,等.超声速燃烧冲压发动机进气道起动性能研究[J].中国空间科学技术,2006,26(6):62-68.
[3] 满延进,李大进,高雄.简单型面调节对高超进气道起动能力影响[C].北京:中国力学大会暨钱学森诞辰100周年纪念大会,2011.
[4] 梁德旺,袁化成,张晓嘉.影响高超声速进气道起动能力的因素分析[J].宇航学报,2006,27(4):714-719.
[5] 刘兴洲.中国超燃冲压发动机研究回顾[J].推进技术,2008,29(4):385-395.(LIUXing-zhou.ReviewofScramjetResearchinChina[J].JournalofPropulsionTechnology,2008,29(4):385-395.)
[6] KantrowitzA,DonaldsonC.PreliminaryInvestigationofSupersonicDiffuser[R].NACAWRL-713,1945.
[7] VanWieDM,KwokFT,WalshRF.StartingCharacteristicsofSupersonicInlets[R].AIAA96-2914.
[8] TimofeevE,TahirR.OnRecentDevelopmentRelatedtoFlowStartinginHypersonicAirIntake[R].AIAA2008-2512
[9] GraingerAL,BrieschenkS,BoyceRR,etal.RotatingInvestigationintotheFlowPhysicsofHypersonicVariableGeometryInletStarting[R].AIAA2014-3230.
[10] NajafiyazdiA.TheoreticalandNumericalAnalysisofSupersonicInletStartingbyMassSpillage[M].Montreal:McGillUniversity,2007.
[11] GraingerAL,BoyceRR,TirteySC,etal.TheUnsteadyFlowPhysicsofHypersonicInletStartingProcesses[R].AIAA2012-5937.
[12] OgawaH,GraingerAL,BoyceRR.InletStartingofHigh-ContractionAxisymmetricScramjets[R].AIAA2009-7401.
[13] HagenmaierMA,TarnCJ,ChakravarthyS.StudyofMovingStartDoorFlowPhysicsforScramjet[R].AIAA99-4957.
[14] Chung-JenTam,MarkAHagenmaier.UnsteadyAnalysisofScramjetInletFlowfieldsUsingNumericalSimulation[R].AIAA99-0613.
[15] 袁化成,梁德旺.高超声速进气道再起动特性分析[J].推进技术,2006,27(5):390-393.(YUANHuacheng,LIANGDe-wang.AnalysisofCharacteristicsofRestartPerformanceforaHypersonicInlet[J].JournalofPropulsionTechnology,2006,27(5):390-393.)(编辑:史亚红)
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