Fuel/air mixing characteristics of scramjet combustor based on acetone⁃PLIF technology

Linsen WANG; Xiaobo TU; Yuhang WANG; Shuang CHEN; Wenyan SONG; Shunhua YANG

doi:10.13224/j.cnki.jasp.20200444

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Fuel/air mixing characteristics of scramjet combustor based on acetone⁃PLIF technology

Combustion, Heat and Mass Transfer | 更新时间：2025-04-07

- Fuel/air mixing characteristics of scramjet combustor based on acetone⁃PLIF technology
- Journal of Aerospace Power Vol. 36, Issue 8, Pages: 1614-1620(2021)
- 作者机构：
  
  1.中国空气动力研究与发展中心高超声速冲压发动机技术重点实验室，四川绵阳 621000
  2.中国空气动力研究与发展中心设备设计与测试技术研究所，四川绵阳 621000
  3.西北工业大学动力与能源学院，西安 710072
- 作者简介：
- 基金信息：
- DOI：10.13224/j.cnki.jasp.20200444
  CLC：
- 稿件说明：
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Linsen WANG, Xiaobo TU, Yuhang WANG, et al. Fuel/air mixing characteristics of scramjet combustor based on acetone⁃PLIF technology[J]. Journal of Aerospace Power, 2021, 36(8): 1614-1620.
DOI：

Linsen WANG, Xiaobo TU, Yuhang WANG, et al. Fuel/air mixing characteristics of scramjet combustor based on acetone⁃PLIF technology[J]. Journal of Aerospace Power, 2021, 36(8): 1614-1620. DOI： 10.13224/j.cnki.jasp.20200444.

摘要

针对超燃冲压发动机燃烧室内燃料/空气掺混特性，设计了一套以acetone⁃PLIF（planar laser⁃induced fluorescence）为技术手段的流动显示测量系统，得到了4种不同结构交错楔形支板在不同特征截面处的丙酮荧光图像，研究了喷嘴位置和尾缘角这两个变量对燃料/空气掺混效果的影响。结果表明：“基准”支板NL1的流场结构主体上表现为横向“S”形曲线，燃料/空气的掺混效果相对普通；NL2支板虽然增大了一些丙酮的扩散范围，但有荧光信号的掺混区域面积却反而有所下降；而引入扩张型尾缘角变量的EL1支板则是大幅改善了燃料/空气的掺混效果，54 mm截面的丙酮分子充满了较大片区域，掺混区域超过截面的1/2。

Abstract

In order to study fuel/air mixing characteristics in scramjet combustor，a non-invasive flow visualization system was designed based on acetone-PLIF （planar laser-induced fluorescence） technology.The acetone fluorescence images of four kinds of shaped struts were obtained at different sections，and the effects of nozzle position and trailing edge angle on fuel/air mixing were studied.The results showed that the flow field of the “standard” NL1 strut was of a transverse “S” curve，which had normal mixing effect in the four struts.The NL2 strut increased a few acetone diffusion range，but decreased mixing area with fluorescence signals.The EL1 strut with an expanded trailing edge angle can greatly improve effect，since the acetone molecules filled over a half of the cross section at 54 mm downstream the strut.

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references

张俊 , 陈柳君 , 胥頔 , 等 . 航空涡轮发动机燃烧室内流程的PIV测量 [J]. 航空动力学报 , 2017 , 32 ( 6 ): 1289 ⁃ 1295 .

ZHANG Jun , CHEN Liujun , XU Di , et al . PIV measurement for inner flow field in aero turbine engine combustor [J]. Journal of Aerospace Power , 2017 , 32 ( 6 ): 1289 ⁃ 1295 . (in Chinese)

刘小勇 . 超燃冲压发动机技术 [J]. 飞弹导弹 , 2005 （ 2 ）: 38 ⁃ 42 .

LIU Xiaoyong . Technology of scramjet [J]. Aerodynamic Missile Journal , 2005 （ 2 ）: 38 ⁃ 42 . (in Chinese)

贺武生 . 超燃冲压发动机研究综述 [J]. 火箭推进 , 2005 , 31 ( 1 ): 29 ⁃ 32 .

HE Wusheng . Research review of scramjet [J]. Journal of Rocket Propulsion , 2005 , 31 ( 1 ): 29 ⁃ 32 . (in Chinese)

李建平 , 宋文艳 , 肖隐利 . 超燃冲压发动机/机体一体化优化设计 [J]. 航空动力学报 , 2011 , 26 ( 4 ): 874 ⁃ 879 .

LI Jianping , SONG Wenyan , XIAO Yinli . Research on the optimization design of integrated scramjet/airframe [J]. Journal of Aerospace Power , 2011 , 26 ( 4 ): 874 ⁃ 879 . (in Chinese)

鲍文 , 郭林春 , 崔涛 , 等 . 超燃冲压发动机燃烧室传感器最佳位置选择 [J]. 航空动力学报 , 2007 , 22 ( 3 ): 475 ⁃ 479 .

BAO Wen , GUO Linchun , CUI Tao , et al . Optimal sensor location of scramjet combustor [J]. Journal of Aerospace Power , 2007 , 22 ( 3 ): 475 ⁃ 479 . (in Chinese)

BAKOS R J ， TAMAGNO , J ， RIZKALLA O ， et al . Hypersonic mixing and combustion studies in the hypulse facility [J]. Journal of Propulsion and Power , 1992 , 8 ( 4 ): 900 ⁃ 906 .

迟鸿伟 , 魏志军 , 李彪 , 等 . 燃烧室构型对固体燃料超燃冲压发动机自点火的影响 [J]. 航空动力学报 , 2016 , 31 ( 8 ): 1985 ⁃ 1994 .

CHI Hongwei , WEI Zhijun , LI Biao , et al . Influence of combustor shape on self⁃ignition in solid fuel scramjet [J]. Journal of Aerospace Power , 2016 , 31 ( 8 ): 1985 ⁃ 1994 . (in Chinese)

REID J Z ， LYNCH K P ， THUROW B S . Density measurements of a high⁃speed,compressible flow field using acetone planer laser induced fluorescence [R]. AIAA⁃2011⁃987 ， 2011 .

BUSA K M ， BRYNER E ， MCDANIEL J C ， et al . Demonstration of capability of water flux measurement in a scramjet combustor using tunable diode laser absorption tomography and stereoscopic PIV [R]. AIAA⁃2011⁃1294 ， 2011 .

CUTLER A D , MAGNOTTI G ， CANTU L ， et al . Dual⁃pump CARS measurements in the University of Virginia's dual⁃mode scramjet:configuration “A” [R]. AIAA⁃2012⁃0114 ， 2012 .

KIDD F G , DANEHY P M , CABELL K F , et al . Characterization of the NASA Langley arc heated scramjet test facility using NO PLIF [R]. AIAA⁃2014⁃2652 ， 2014 .

ALLISON P , FREDERICKSON K , KIRIK J W , et al . Investigation of flame structure and combustion dynamics using CH 2 O PLIF and high⁃speed CH chemiluminescence in premixed dual⁃mode scramjet combustor [R]. AIAA⁃2016⁃0441 ， 2016 .

RANKIN B A , FUGGER C A , RICHARDSON D R . Evaluation of mixing processes in a non⁃premixed rotating detonation engine using acetone PLIF imaging [R]. AIAA⁃2016⁃1198 ， 2016 .

杨国华 , 洪流 , 李鳌 , 等 . 丙酮平面激光诱导荧光技术在喷嘴混合研究中的应用 [J]. 实验流体力学 , 2008 , 22 ( 4 ): 23 ⁃ 28 .

YANG Guohua , HONG Liu , LI Ao , et al . Application of acetone planar laser⁃induced fluorescence in research on mixing characteristics of injector [J]. Journal of Experiments in Fluid Mechanics , 2008 , 22 ( 4 ): 23 ⁃ 28 . (in Chinese)

俞瑜 . 气体引射式无焰燃烧的数值模拟和实验研究 [D]. 合肥 : 中国科学技术大学 , 2010 .

YU Yu . Experimental study and numerical simulation of gas flameless combustion induced by the inner structure [D]. Hefei : University of Science and Technology of China , 2010 . (in Chinese)

刘存喜 , 刘富强 , 毛艳辉 , 等 . 某型航空发动机用离心喷嘴燃油空间分布特性试验 [J]. 航空动力学报 , 2013 , 28 ( 4 ): 783 ⁃ 791 .

LIU Cunxi , LIU Fuqiang , MAO Yanhui , et al . Experiment of fuel distribution of pressure⁃swirl atomizers for aero⁃engine [J]. Journal of Aerospace Power , 2013 , 28 ( 4 ): 783 ⁃ 791 . (in Chinese)

周淼 . 基于丙酮平面激光诱导荧光气流混合比测量研究 [D]. 哈尔滨 : 哈尔滨工业大学 , 2015 .

ZHOU Miao . Research on measurements of air mixing ratio using acetone planar laser induced fluorescence [D]. Harbin : Harbin Institute of Technology , 2015 . (in Chinese)

严浩 , 张少华 , 余西龙 , 等 . OH与CH 2 O双组分平面激光诱导荧光对旋流燃烧室火焰结构与脉动特征的研究 [J]. 航空动力学报 , 2019 , 34 ( 4 ): 894 ⁃ 907 .

YAN Hao , ZHANG Shaohua , YU Xilong , et al . Flame structure and dynamics characters investigation by OH and CH 2 O planner laser⁃induced fluorescence in the swirl combustor [J]. Journal of Aerospace Power , 2019 , 34 ( 4 ): 894 ⁃ 907 . (in Chinese)

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