| Citation: | Experiment on supersonic reacting mixing layer of splitters with different geometric configurations[J]. Journal of Aerospace Power, 2017, 32(1): 27-34. doi: 10.13224/j.cnki.jasp.2017.01.005
|
| [1] |
Miller M F I T C,Yip B,Bowman C T.An experimental study of the structure of a compressible,reacting mixing layer［R］.AIAA 930354,1993.
|
| [2] |
Miller M F I T C,Seitzman J M.Compressibility effects in areacting mixing layer［R］.AIAA 931771,1993.
|
| [3] |
Miller M F I T C,Seitzman J M.An experimental investigation of supersonic reacting mixing layers［R］.AIAA 940823,1994
|
| [4] |
Hall J L.An experimental investigation of structure,mixing and combustion in compressible turbulent shear layers［M］.Belvoir:Defense Technical Information Center，1991.
|
| [5] |
Barlow R S,Fourguette D C,Mungal M G,et al.Experiments on the structure of an annular compressible reacting shear layer［J］.AIAA Journal,1992,30(9):2244-2251.
|
| [6] |
刘彧,周进,晏至辉.不同隔板构型下的超声速混合层流场特性［J］.国防科学技术大学学报，2013,35(5):1-5. LIU Yu,ZHOU Jin,YAN Zhihui.Study on the flow fields of supersonic mixing layer with splitters of different geometric configurations［J］.Journal of National University of Defense Technology,2013,35(5):1-5.(in Chinese)
|
| [7] |
刘彧.双燃烧室冲压发动机混合增强及燃烧流场的实验和数值仿真研究［D］.长沙:国防科学技术大学,2011. LIU Yu.An experimental and numerical investigation of mixing enhancement and combusting flow field of dual combustor ramjet［D］.Changsha:National University of Defense Technology,2011.(in Chinese)
|
| [8] |
Rogers R C C D,Pa G R W.Experimental supersonic combustion research at NASA Langley［R］.AIAA 982506,1998.
|
| [9] |
Seiner J M G G E.Effect of tabs on mixing on round jets［R］.AIAA 982326,1998.
|
| [10] |
Yu K H S K C.Role of large coherent structures in turbulent compressible mixing［J］.Experimental Thermal and Fluid Science,1997,14(1):75-84.
|
| [11] |
于江飞，晏至辉，刘卫东.双燃烧室冲压发动机三维隔板后缘构型数值研究［J］.弹箭与制导学报,2010,30(4):108-112. YU Jiangfei,YAN Zhihui,LIU Weidong.Numerical study for threedimensional clap board models in dual combustor ramjet［J］.Jounal of Projectiles Rockets Missiles and Guidance,2010,30(4):108-112.(in Chinese)
|
| [12] |
晏至辉.超声速混合层混合、燃烧机理研究［D］.长沙：国防科学技术大学，2013. YAN Zhihui.Investigations on mixing and combustion mechanism of supersonic mixing layers［D］.Changsha:National University of Defense Technology,2013.(in Chinese)
|
| [13] |
晏至辉.双燃烧室冲压发动机超声速混合层混合增强数值研究［J］.航空动力学报，2010,25(4):821-828. YAN Zhihui.Numerical study on mixing enhancement for supersonic mixing layer in dual combustor ramjet［J］.Journal of Aerospace Power，2010,25(4):821-828.(in Chinese)
|
| [14] |
耿辉,翟振辰,桑艳,等.利用OHPLIF技术显示超声速燃烧的火焰结构［J］.国防科学技术大学学报，2006,28(2):1-6. GENG Hui,ZHAI Zhenchen,SANG Yan,et al.Reveal the flame structure of supersonic combustion using OHPLIF technology［J］.Journal of National University Defense Technology,2006,28(2):1-6.(in Chinese)
|
| [15] |
李麦亮.激光光谱诊断技术及其在火箭发动机燃烧研究中的应用［D］.长沙:国防科学技术大学，2004. LI Mailiang.Studies on laser spectroscopy technology and its application to combustion diagnosis in the jet engine［D］.Changsha:National University Defense Technology,2004.(in Chinese)
|
| [16] |
耿辉.超声速燃烧室中凹腔上游横向喷注燃料的流动、混合与燃烧特性研究［D］.长沙:国防科学技术大学，2007. GENG Hui.Investigation of flow,mixing and combustion properties of transverse fuel injection up stream of the cavity in a supersonic combustor［D］.Changsha:National University Defense Technology,2007.(in Chinese)
|
| [17] |
范周琴.超声速湍流燃烧火焰面模型判别、建模及应用研究［D］.长沙:国防科学技术大学,2011. FAN Zhouqin.Investigation of validation,modeling cation of flamelet model in supersonic turbulent combustion［D］.Changsha:National University Defense Technology,2011.(in Chinese)
|
DownLoad: