| Citation: | TIAN Liang, XU Xu, ZHU Shao-hua. Influence of injection location on upstream struts in a dual-struts supersonic combustor[J]. Journal of Aerospace Power, 2016, 31(11): 2613-2620. doi: 10.13224/j.cnki.jasp.2016.11.007
|
| [1] |
俞刚,范学军.超声速燃烧与高超声速推进[J].力学进展,2013,43(5):449-471. YU Gang,FAN Xuejun.Supersonic combustion and hypersonic propulsion[J].Advances in Mechanics,2013,43(5):449-471.(in Chinese)
|
| [2] |
ZHANG Taichang,YUAN Yueming,LI Jianguo,et al.Characteristics of a supersonic model combustor with two-staged injections of supercritical kerosene[R].AIAA-2012-3762,2012.
|
| [3] |
Sadatake T,Atsuo M,Kenji K,et al.Effects of injection scheme on performance of a staged supersonic combustor[R].AIAA 99-2107,1999.
|
| [4] |
Sadatake T,Atsuo M,Kenji K,et al.Combustion tests of a staged supersonic combustor with a strut[J].Journal of Propulsion and Power,2001,17(2):293-300.
|
| [5] |
Sadatake T,Kan K,Kenji K,et al.Distributed injection for performance improvement of a supersonic combustor with multi-staged wall injections[R].AIAA-2003-6991,2003.
|
| [6] |
Vellaramkalayil J J,Scheuermann T,von Wolfersdorf J.analysis of a two-staged supersonic combustion chamber using experiments and simulations[R].AIAA-2011-2247,2011.
|
| [7] |
Sirka F,Andreas H,Hans P K.The investigations on multi-stage supersonic combustion in a model combustor[R].AIAA-2011-2332,2011.
|
| [8] |
刘世杰,潘余,刘卫东.超燃冲压发动机支板喷射燃料的燃烧过程试验[J].航空动力学报,2009,24(1):55-59. LIU Shijie,PAN Yu,LIU Weidong.Experimental study on the combustion and flow process in a scramjet with strut injector[J].Journal of Aerospace Power,2009,24(1):55-59.(in Chinese)
|
| [9] |
刘世杰,潘余,刘卫东.带支板超燃冲压发动机燃烧流动过程试验研究[J].弹箭与制导学报,2009,29(1):166-172. LIU Shijie,PAN Yu,LIU Weidong.Combustion tests of a scramjet combustor with a strut[J].Journal of Projectiles,Rockets,Missiles and Guidance,2009,29(1):166-172.(in Chinese)
|
| [10] |
苏义,刘卫东.支板超声速冷流流场及液体喷流混合特性[J].推进技术,2009,30(6):661-665. SU Yi,LIU Weidong.Investigation on supersonic cold flow and liquid jet over struts[J].Journal of Propulsion Technology,2009,30(6):661-665.(in Chinese)
|
| [11] |
范周琴,刘卫东,林志勇,等.支板喷射超声速燃烧火焰结构实验[J].推进技术,2012,33(6):923-927. FAN Zhouqin,LIU Weidong,LIN Zhiyong,et al.Experimental investigation of supersonic combustion flame structure with strut injectors[J].Journal of Propulsion Technology,2012,33(6):923-927.(in Chinese)
|
| [12] |
徐朝启,何国强,刘佩进,等RBCC发动机亚燃模态一次火箭引导燃烧的实验[J].航空动力学报,2013,28(3):567-572. XU Chaoqi,HE Guoqing,LIU Peijin,etal.Experiments of primary rocket-piloting combustion under ramjet-mode condition in RBCC[J].Journal of Aerospace power,2013,28(3):567-572.(in Chinese)
|
| [13] |
程诚,覃粒子,刘宇.基于支板燃烧室的喷管化学非平衡效应[J].北京航空航天大学学报,2013,39(1):31-36. CHENG Cheng,QIN Lizi,LIU Yu.Nozzle chemical non-equilibrium effects based on strut combustor[J].Journal of Beijing University of Aeronautics and Astonautics,2013,39(1):31-36.(in Chinese)
|
| [14] |
何国强,徐朝起,秦飞,等.基于直扩流道构型的RBCC发动机亚燃模态高效燃烧组织研究[J].推进技术,2013,34(8):1064-1070. HE Guoqiang,XU Chaoqi,QIN Fei,et al.Research on ramjet-mode combustion organization based on constant-expansion configuration in RBCC combustor[J]. Journal of Propulsion Technology,2013,34(8):1064-1070.(in Chinese)
|
| [15] |
冮强,周乐仪,覃正,等.液体碳氢燃料超燃冲压发动机支板凹槽稳焰技术试验[J].推进技术,2011,32(5):680-683. GANG Qiang,ZHOU Leyi,QIN Zheng,et al.Experimental investigation of strut-cavity flame-holder technology in liquid hydrocarbon fueled scramjet combustor[J].Journal of Propulsion Technology,2011,32(5):680-683.(in Chinese)
|
| [16] |
潘科玮,何国强,秦飞,等.煤油燃料RBCC亚燃模态掺混与燃烧数值模拟研究[J].推进技术,2012,33(6):907-913. PAN Kewei,HE Guoqiang,QIN Fei,et al.Study on mixing and combustion of kerosene fuel in ramjet mode of RBCC engine[J].Journal of Propulsion Technology,2012,33(6):907-913.(in Chinese)
|
| [17] |
Kumaran K,Babu V.Mixing and combustion characteristics of kerosene in a model supersonic combustor[J].Journal of Propulsion and Power,2009,25(3):583-592.
|
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