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连续旋转爆震波的瞬时传播特性

王超 刘卫东 刘世杰 林志勇 蒋露欣

王超, 刘卫东, 刘世杰, 林志勇, 蒋露欣. 连续旋转爆震波的瞬时传播特性[J]. 航空动力学报, 2015, 30(11): 2600-2606. doi: 10.13224/j.cnki.jasp.2015.11.006
引用本文: 王超, 刘卫东, 刘世杰, 林志勇, 蒋露欣. 连续旋转爆震波的瞬时传播特性[J]. 航空动力学报, 2015, 30(11): 2600-2606. doi: 10.13224/j.cnki.jasp.2015.11.006
WANG Chao, LIU Wei-dong, LIU Shi-jie, LIN Zhi-yong, JIANG Lu-xin. Instantaneous propagation characteristics of continuous rotating detonation wave[J]. Journal of Aerospace Power, 2015, 30(11): 2600-2606. doi: 10.13224/j.cnki.jasp.2015.11.006
Citation: WANG Chao, LIU Wei-dong, LIU Shi-jie, LIN Zhi-yong, JIANG Lu-xin. Instantaneous propagation characteristics of continuous rotating detonation wave[J]. Journal of Aerospace Power, 2015, 30(11): 2600-2606. doi: 10.13224/j.cnki.jasp.2015.11.006

连续旋转爆震波的瞬时传播特性

doi: 10.13224/j.cnki.jasp.2015.11.006
基金项目: 

国家自然科学基金(51306202,91216120)

详细信息
    作者简介:

    王超(1987-),男,湖北蕲春人,博士生,研究领域为连续旋转爆震.

  • 中图分类号: V231.2

Instantaneous propagation characteristics of continuous rotating detonation wave

  • 摘要: 开展氢气/空气连续旋转爆震试验,并计算连续旋转爆震波的瞬时传播频率与传播速度,统计其相对标准偏差,并以此作为爆震波瞬时传播过程稳定性的评价标准,研究推进剂流量对连续旋转爆震波瞬时传播特性的影响.结果表明:在当量比为1.0时,空气流量由321g/s增加至505g/s,连续旋转爆震波的平均传播频率由4.60kHz升高至5.33kHz,平均传播速度由1445m/s增加为1674m/s;连续旋转爆震波瞬时传播频率的相对标准偏差则由4.00%减小至1.69%,这表明连续旋转爆震波在较大的推进剂流量下的传播过程更加稳定.

     

  • [1] Kailasanath K.Review of propulsion applications of detonation waves[J].AIAA Journal,2000,38(9):1698-1708.
    [2] Lu F K,Braun E M,Massa L,et al.Rotating detonation wave propulsion:experimental challenges,modeling,and engine concepts (invited)[R].AIAA-2011-6043,2011.
    [3] SHAO Yetao,WANG Jianping.Change in continuous detonation wave propagation mode from rotating detonation to standing detonation[J].Chinese Physics Letters,2010,27(3):034705.1-034705.4.
    [4] Bykovskii F A,Zhdan S A,Vedernikov E F.Reactive thrust generated by continuous detonation in the air ejection mode[J].Combustion,Explosion,and Shock Waves,2013,49(2):188-195.
    [5] Bykovskii F A,Zhdan S A,Vedernikov E F.Continuous spin detonation of fuel-air mixtures[J].Combustion,Explosion,and Shock Waves,2006,42(4):463-471.
    [6] Wolański P.Detonative propulsion[J].Proceedings of the Combustion Institute,2013,34(1):125-158.
    [7] Bykovskii F A,Vedernikov E F.Continuous detonation of a subsonic flow of a propellant[J].Combustion,Explosion,and Shock Waves,2003,39(3):323-334.
    [8] Dyer R,Naples A,Kaemming T,et al.Parametric testing of a unique rotating detonation engine design[R].AIAA-2012-0121,2012.
    [9] 刘世杰,林志勇,林伟,等.H2/Air连续旋转爆震波的起爆及传播过程试验[J].推进技术,2012,33(3):483-489. LIU Shijie,LIN Zhiyong,LIN Wei,et al.Experiment on the ignition and propagation processes of H2/Air continuous rotating detonation wave[J].Journal of Propulsion Technology,2012,33(3):483-489.(in Chinese)
    [10] 刘世杰,刘卫东,林志勇,等.连续旋转爆震波传播过程研究:Ⅰ 同向传播模式[J].推进技术,2014,35(1):138-144. LIU Shijie,LIU Weidong,LIN Zhiyong,et al.Research on continuous rotating detonation wave propagation process:Ⅰ one direction mode[J].Journal of Propulsion Technology,2014,35(1):138-144.(in Chinese)
    [11] 刘世杰,林志勇,刘卫东,等.连续旋转爆震波传播过程研究:Ⅱ 双波对撞传播模式[J].推进技术,2014,35(2):269-275. LIU Shijie,LIN Zhiyong,LIU Weidong,et al.Research on continuous rotating detonation wave propagation process:Ⅱ two-wave collision propagation mode[J].Journal of Propulsion Technology,2014,35(2):269-275.(in Chinese)
    [12] ZHENG Quan,WENG Chunsheng,BAI Qiaodong.Experimental research on the propagation process of continuous rotating detonation wave[J].Defence Technology,2013,9(4):201-207.
    [13] Suchocki J A,Yu S T J,Hoke J L,et al.Rotating detonation engine operation[R].AIAA-2012-0119,2012.
    [14] 唐新猛,王健平,邵业涛.连续旋转爆轰波在无内柱圆筒内的数值模拟[J].航空动力学报,2013,28(4):792-799. TANG Xinmeng,WANG Jianping,SHAO Yetao.3-D simulation of rotating detonation wave in combustor chamber without inner wall[J].Journal of Aerospace Power,2013,28(4):792-799.(in Chinese)
    [15] Kindracki J,Kobiera A,Wolanski P,et al.Experimental and numerical study of the rotating detonation engine in hydrogen air mixtures[J].Progress in Propulsion Physics,2011,2:555-582.
    [16] WANG Yuhui,WANG Jianping,SHI Tianyi,et al.Discovery of breathing phenomena in continuously rotating detonation[J].Procedia Engineering,2013,67:188-196.
    [17] 姜孝海,范宝春,董刚,等.旋转爆轰流场的数值模拟[J].推进技术,2007,28(4):403-407. JIANG Xiaohai,FAN Baochun,DONG Gang,et al.Numerical investigation on the flow field of rotating detonation wave[J].Journal of Propulsion Technology,2007,28(4):403-407.(in Chinese)
    [18] Tsuboi N,Hayashi A K,Koshi M.Energy release effect of mixture on single spinning detonation structure[J]. Proceedings of the Combustion Institute,2009,32(1):2405-2412.
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出版历程
  • 收稿日期:  2014-05-03
  • 刊出日期:  2015-11-28

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