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射流自由长度对凝胶推进剂撞击雾化影响的实验

邓寒玉 封锋

邓寒玉, 封锋. 射流自由长度对凝胶推进剂撞击雾化影响的实验[J]. 航空动力学报, 2018, 33(1): 215-222. doi: 10.13224/j.cnki.jasp.2018.01.026
引用本文: 邓寒玉, 封锋. 射流自由长度对凝胶推进剂撞击雾化影响的实验[J]. 航空动力学报, 2018, 33(1): 215-222. doi: 10.13224/j.cnki.jasp.2018.01.026
Experiment on effect of free jet length on impinging atomization of gel propellant[J]. Journal of Aerospace Power, 2018, 33(1): 215-222. doi: 10.13224/j.cnki.jasp.2018.01.026
Citation: Experiment on effect of free jet length on impinging atomization of gel propellant[J]. Journal of Aerospace Power, 2018, 33(1): 215-222. doi: 10.13224/j.cnki.jasp.2018.01.026

射流自由长度对凝胶推进剂撞击雾化影响的实验

doi: 10.13224/j.cnki.jasp.2018.01.026
基金项目: 航天科技创新基金(CASC03-02); 中央高校基本科研业务费专项基金(30920140112001)

Experiment on effect of free jet length on impinging atomization of gel propellant

  • 摘要: 为研究射流自由长度对凝胶推进剂撞击雾化的影响,建立了撞击雾化实验台,制备了煤油凝胶和水基模拟液,测试了雾化装置的喷射系数及模拟液的黏性和稳定性。分析了3种射流速度不同射流自由长度条件下的凝胶撞击雾化特性,观测了射流和撞击喷雾图像。测量了液膜破碎长度、雾化液滴粒径分布和相应的SMD(索太尔平均直径)值。研究结果表明:低速时,随着射流自由长度增大,撞击液膜的喷雾形态会发生较大变化,而高速条件下,雾化形态则基本一致。3种射流速度下,破碎长度在45~9mm之间,并随射流自由长度逐渐减小。液滴分布服从RosinRammler规律,并具有较高的拟合精度。均匀度指数均在3~4之间,并随射流自由长度逐渐降低,粒径均匀度降低;较高射流速度下,SMD随自由长度逐渐增大。低射流速度时,SMD随射流长度先减小后增大,射流自由长度存在一个最优值,在设定研究条件下其值为25/3。因此,在设计撞击喷嘴时,根据射流速度选取适当的自由长度值可以获得更好的雾化效果。

     

  • [1] 刘虎,强洪夫,王广.凝胶推进剂射流撞击雾化研究进展[J].含能材料,2015,23(7):697-708.LIU Hu,QIANG Hongfu,WANG Guang.Review on jet impingement atomization of gelled propellant[J].Chinese Journal of Energetic Materials,2015,23(7):697-708.(in Chinese)
    [2] JAYAPRAKASH N,CHAKRAVARTHY S R.Impingement atomization of gel fuels[R].AIAA2003-316,2003.
    [3] 李建军,夏振炎,田砚.幂律流体撞击射流破碎机理的实验[J].航空动力学报,2015,30(7):1752-1758.LI Jianjun,XIA Zhenyan,TIAN Yan.Experiment on breakup mechanism of impinging jet of powerlaw liquid[J].Journal of Aerospace Power,2015,30(7):1752-1758.(in Chinese)
    [4] 李龙飞,张蒙正,杨伟东,等.喷嘴形式对幂律型非牛顿推进剂雾化特性的影响[J].航空动力学报,2014,29(12):2987-2992.LI Longfei,ZHANG Mengzheng,YANG Weidong,et al.Effects of different injectors on spray characteristics of powerlaw nonNewtonian propellant[J].Journal of Aerospace Power,2014,29(12):2987-2992.(in Chinese)
    [5] FU Q,YANG L,CUI K,et al.Effects of orifice geometry on gelled propellants sprayed from impingingjet injectors[J].Journal of Propulsion and Power,2014,30(4):1113-1117.
    [6] JUNG K,KHIL T,YOON Y.Effect of internal flow on mixing in the spray form a pair of unlike impinging jet[J].Journal of Spacecraft and Rockets,2006,22(3):653-660.
    [7] INAMURA T,SHIROTA M.Effect of velocity profile of impinging jets on sheet characteristics formed by impingement of two round liquid jets[J].International Journal of Multiphase Flow,2014,60:149-160.
    [8] RAHIMI S,NATAN B.Airblast atomization of gel fuels[R].AIAA2001-3276,2001.
    [9] AVULAPATI M M,VENKATA R R.Experimental studies on airassisted impinging jet atomization[J].International Journal of Multiphase Flow,2013,57:88-101.
    [10] MALLORY J A,SOJKA P E.Impinging jet structure and breakup using gelled propellant simulant[R].Estoril,Portugal:24th European Conference on Liquid Atomization and Spray Systems,2011.
    [11] REN N,MARSHALL A W.Characterizing the initial spray from large Weber number impinging jets[J].International Journal of Multiphase Flow,2014,58:205-213.
    [12] RAHIMI S,HASAN D,PERETZ A,et al.Preparation and characterisztion of gel propellants and simulants[R].AIAA2001-3264,2001.
    [13] ARNOLD R,SANTOS P H S,CAMPANELLA O H,et al.Rheological and thermal behavior of gelled hydrocarbon fuels[J].Journal of Propulsion and Power,2011,27(1):151-162.
    [14] OCHOWIAK M,BRONIARZPRESS L,WOZIWODZKI S.The analysis of silica suspensions atomization[J].International Journal of Heat and Fluid Flow,2011,32(6):1208-1215.
    [15] 强洪夫,夏学礼.凝胶推进剂管道流动特性影响因素数值分析[J].含能材料,2009,17(2):137-142.QIANG Hongfu,XIA Xueli.Numerical analysis of factors affecting flow property of gel propellants in round pipes[J].Chinese Journal of Energetic Materials,2009,17(2):137-142.(in Chinese)
    [16] 曹琪,封锋,武晓松,等.凝胶推进剂供给管流的压降数值研究[J].推进技术,2014,35(5):701-707.CAO Qi,FENG Feng,WU Xiaosong,et al.Numerical study on pressure loss for gel propellants supply pipeline[J].Journal of Propulsion Technology,2014,35(5):701-707.(in Chinese)
    [17] CHOJNACKI K T,FEIKEIKEMA D A.Study of nonNewtonian liquid sheets formed by impinging jets[R].AIAA 97-3335,1997.
    [18] HEISLBETZ B,MADLENER K,CIEZKI H K.Breakup characteristics of a Newtonian liquid sheet formed by a doublet impinging jet injector[R].AIAA2007-5694,2007.
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出版历程
  • 收稿日期:  2016-06-20
  • 刊出日期:  2018-01-28

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