[1]王 政,张 涵,龙振国,等.军用高超飞行器超燃燃烧室悬臂斜坡喷注器喷注方式优化[J].弹箭与制导学报,2017,37(5):81-86.[doi:10.15892/j.cnki.djzdxb.2017.05.001]
 WANG Zheng,ZHANG Han,LONG Zhenguo,et al.Optimization of Spray Injection Mode for Cantilever Slope Sprayer of Military Super-aircraft[J].,2017,37(5):81-86.[doi:10.15892/j.cnki.djzdxb.2017.05.001]
点击复制

军用高超飞行器超燃燃烧室悬臂斜坡喷注器喷注方式优化

参考文献/References:

[1] 徐旭, 陈兵, 徐大军. 冲压发动机原理及技术 [M]. 北京: 北京航空航天大学出版社, 2014: 175-200.
[2] CURRAN E T, MURTHY S N B. Scramjet propulsion [M]. Reston:AIAA, 2002: 28-44.
[3] 金亮, 黄伟, 郭善广. 超燃冲压发动机旋转斜坡概念研究 [J]. 推进技术, 2014, 35(4): 530-536.
[4] SISLIAN J P, SCHUMACHER J. A comparative study of hypersonic fuel/air mixing enhancement by ramp and cantilevered ramp injectors: AIAA 99-4873 [R].[S.l.:s.n.], 1999.
[5] WANG Y W, SISLIAN J P. Numerical investigation of methane and air mixing in a shcramjet inlet:AIAA 2008-2533[R]. Reston:AIAA, 2008.
[6] SISLIAN J P, PARENT B. Hypervelocity fuel/air mixing in a shcramjet inlet [J]. Journal of Propul and Power, 2004, 20(2): 263-272.
[7] PARENT B, SISLIAN J P. Effect of geometrical parameters on the mixing performance of cantilevered ramp injectors [J]. AIAA Journal, 2003, 41(3): 448-456.
[8] WANG Y W, SISLIAN J P. Numerical investigation of methaneand air mixing in a shcramjet inlet: AIAA 2008-2533 [R].[S.l.]: AIAA, 2008.
[9] HUANG Wei, LI Shi-bin, YAN Li, et al. Performance evaluation and parametric analysis on cantilevered ramp injector in supersonic flows [J]. Acta Astronautica,2013,84:141-152.
[10] 杨银军, 窦志国, 段立伟. 超声速来流中横向喷流角度对流动与混合特性的影响 [J]. 现代电子技术, 2013, 36(17): 151-154.
[11] OGAWA H, BOYEE R R. Computational investigation of fuel injection with various injector geometries and mixing into hypersonic cross flow in scramjet engines Grapevine, Texas: AIAA 2013-0115 [R]. [S.l.]: AIAA, 2013.
[12] POHLMAN M R. GREEND KE R B. Critical design parameters for pylon-aided gaseous fuel injection: AIAA 2009-1422[R]. [S.l.] AIAA, 2009.
[13] 闫明磊, 韦宝禧, 徐旭, 等. 应用气动斜坡和燃气发生器的超燃烧室 [J]. 北京航空航天大学学报, 2011, 37(7): 782-788.
[14] SEGAL Corin. The scramjet engine:processes and characteristics [M]. Cambridge: Cambridge University Press, 2009: 85-86.
[15] WEI Baoxi, ZHANG yan, TIAN Liang, et al. Experimental study on combustion mode transition in an aero-ramp based scramjet: Atlanta. Georgia: AIAA 2012-3923 [R]. Reston: AIAA, 2012.
[16] MONTES D R, KING P I. GRUBER M R, et al. Mixing effects of pylon-aided fuel injection located upstream of flame holding cavity in supersonic flow: AIAA 2005-3913 [R]. Reston: AIAAA, 2005.

相似文献/References:

[1]王旭东,高 峰,王应洋,等.超燃燃烧室支板喷注器燃料掺混优化数值分析[J].弹箭与制导学报,2016,36(1):93.[doi:10.15892/j.cnki.djzdxb.2016.01.024]
 WANG Xudong,GAO Feng,WANG Yingyang,et al.Numerical Optimization Analysis of Fuelair Mixing for a Supersonic Combustor with Strut Injector[J].,2016,36(5):93.[doi:10.15892/j.cnki.djzdxb.2016.01.024]
[2]张 涵,吴 达,王应洋,等.乙烯超燃燃烧室菱形孔射流的数值优化[J].弹箭与制导学报,2016,36(3):60.[doi:10.15892/j.cnki.djzdxb.2016.03.017]
 ZHANG Han,WU Da,WANG Yingyang,et al.Numerical Optimization on Supersonic Combustion using Ethylene with Diamond-shaped Orifices[J].,2016,36(5):60.[doi:10.15892/j.cnki.djzdxb.2016.03.017]
[3]夏雪峰,高 峰,王宏宇,等.支板构型对煤油/空气混合影响数值分析[J].弹箭与制导学报,2016,36(6):83.[doi:10.15892/j.cnki.djzdxb.2016.06.021]
 XIA Xuefeng,GAO Feng,WANG Hongyu,et al.Numerical Analysis of the Influence of Strut Configuration on the Mixture of Kerosene/Air[J].,2016,36(5):83.[doi:10.15892/j.cnki.djzdxb.2016.06.021]
[4]黄桂彬,吴 达,王应洋,等.超燃燃烧室小支板三维尺寸数值优化[J].弹箭与制导学报,2017,37(1):81.[doi:10.15892/j.cnki.djzdxb.2017.01.019]
 HUANG Guibin,WU Da,WANG Yingyang,et al.Numerical Optimization of Three Dimensional Size of Small Supported Plate in a Scramjet Combustion[J].,2017,37(5):81.[doi:10.15892/j.cnki.djzdxb.2017.01.019]
[5]高 峰,王旭东,王宏宇,等.带并联凹腔的超燃燃烧室数值研究[J].弹箭与制导学报,2017,37(2):0.[doi:10.15892/j.cnki.djzdxb.2017.02.002]
 GAO Feng,WANG Xudong,WANG Hongyu,et al.Numerical Study on Supersonic Combustor using Parallel Cavity[J].,2017,37(5):0.[doi:10.15892/j.cnki.djzdxb.2017.02.002]

备注/Memo

作者简介:王政(1990-),男,山东菏泽人,博士研究生,研究方向:军事作战应用研究。

更新日期/Last Update:

2017-08-15