[1] 林左鸣.战斗机发动机的研制现状和发展趋势[J].航空发动机,2006,32(1):1-8.
[2] 单勇,张靖周,邵万仁,等.某型涡扇排气系统缩比模型红外辐射特性实验[J].航空动力学报,2009,24(10):2228-2234.
[3] KeenerER,SpaidFW.HypersonicNozzle-AfterbodyExperiment:FlowVisualizationandBoundary-LayerMeasurements[J].JournalofSpacecraftandRockets,1996,33(3):326-332.
[4] SpaidFW,KeenerER.HypersonicNozzle-AfterbodyExperiment:FlowfieldSurveys[J].JournalofSpacecraftandRockets,1996,33(3):333-338.
[5] WatanabeS.ScramjetNozzleExperimentwithHypersonicExternalFlow[J].JournalofPropulsionandPower,1993,9(4):521-528.
[6] CaponeFJ,ReRJ,BareEA.ParametricInvestigationofSingle-Expansion-RampNozzlesatMachNumbersfrom0.60to1.20[R].NASATP-3240,1992.
[7] 谭杰,金捷,杜刚,等.下腹板长度对单边膨胀喷管性能的影响[J].航空动力学报,2012,27(4):726-734.
[8] 谭杰,金捷,杜刚,等.单边膨胀喷管试验和数值模拟[J].航空动力学报,2011,26(6):1223-1230.
[9] 谭杰,金捷,杜刚,等.过膨胀单边膨胀喷管试验和数值模拟[J].推进技术,2009,30(3):292-296.(TANJie,JINJie,DUGang,etal.ExperimentalandComputationalInvestigationofanOver-ExpandedSingle-Expansion-Ramp-Nozzle[J].JournalofPropulsionTechnology,2009,30(3):292-296.)
[10] 谭杰,金捷.单边膨胀喷管几何参数对内特性和流场的影响[J].推进技术,2013,34(2):152-160.(TANJie,JINJie.EffectsofGeometricParametersonInternalPerformanceandFlowfieldofSingleExpansionRampNozzles[J].JournalofPropulsionTechnology,2013,34(2):152-160.)
[11] 汪维娜,王占学,乔渭阳.单斜面膨胀喷管几何参数对流场和性能的影响[J].航空动力学报,2006,21(2):280-284.
[12] 李念,张堃元,徐惊雷.二维非对称喷管数值模拟与验证[J].航空动力学报,2004,19(6):802-805.
[13] 张堃元,张荣学,徐辉.非对称大膨胀比喷管研究[J].推进技术,2001,22(5):380-382.(ZHANGKun-yuan,ZHANGRong-xue,XUHui.InvestigationofSingleExpansionRampNozzle[J].JournalofPropulsionTechnology,2001,22(5):380-382.)
[14] BurleyJR,CarlsonJR.Circular-to-RectangularTransitionDuctsforHigh-Aspect-RatioNonaxisymmetricNozzles[R].AIAA85-1346.
[15] Xiang-yuLi,JieJin,GangDu.ExperimentalandNumericalInvestigationonthePerformanceofSingleExpansionRampNozzleofDifferentFlapLength[R].Cairns:APISAT2015,2015.(编辑:梅瑛)
|
