| Citation: | YUAN Xun, YU Xin, PENG Jiangbo, et al. Combustion diagnosis of ramjet in high-enthalpy shock tunnel using high-speed OH-PLIF[J]. Journal of Aerospace Power, 2026, 41（5）：20240647 doi: 10.13224/j.cnki.jasp.20240647
|
To address the research gap in high-frequency planar laser-induced fluorescence (PLIF) combustion diagnostics for high-Mach number scramjet engines, a high-enthalpy shock tunnel high-frequency PLIF measurement system was developed. For the first time, high-frequency OH-PLIF combustion diagnostic tests were conducted under nominal Mach number 10 flight simulation conditions in a free piston-driven high-enthalpy shock tunnel. Time series images of OH-PLIF in the combustion chamber were obtained for both ethylene and hydrogen injection cases. By comparing the background images, it was observed that the test gas reached the engine flow path approximately 8 ms after the tunnel startup for ethylene injection. The OH in the combustion flame was found to be distributed closer to the cowl side, and shock wave structures parallel to the rear edge of the cavity on the compression side were observed within the rectangular flow path. Compared with ethylene injection, hydrogen injection resulted in earlier ignition around 3 ms after tunnel startup due to the ablation effect, leading to a flame distribution that was nearly uniform across the entire field. These findings were in good agreement with the combustion chamber pressure data.
| [1] |
黄刚, 李朗, 田野, 等. 氢燃料超燃冲压发动机燃烧流场结构和性能[J]. 航空动力学报, 2023, 38(9): 2177-2185. HUANG Gang, LI Lang, TIAN Ye, et al. Combustion flow field structure and performance in hydrogen-fueled scramjet[J]. Journal of Aerospace Power, 2023, 38(9): 2177-2185. (in Chinese
HUANG Gang, LI Lang, TIAN Ye, et al. Combustion flow field structure and performance in hydrogen-fueled scramjet[J]. Journal of Aerospace Power, 2023, 38(9): 2177-2185. (in Chinese)
|
| [2] |
张冬青, 邓维鑫, 邢建文, 等. Ma10条件超燃冲压发动机自由射流试验过程[J]. 航空动力学报, 2023, 38(3): 735-742. ZHANG Dongqing, DENG Weixin, XING Jianwen, et al. Scramjet free-jet test process at Ma10 conditions[J]. Journal of Aerospace Power, 2023, 38(3): 735-742. (in Chinese
ZHANG Dongqing, DENG Weixin, XING Jianwen, et al. Scramjet free-jet test process at Ma10 conditions[J]. Journal of Aerospace Power, 2023, 38(3): 735-742. (in Chinese)
|
| [3] |
伍军, 李向东, 蒲旭阳, 等. 燃烧加热类高超声速高温风洞流场校测与评估[J]. 推进技术, 2022, 43(10): 210122. WU Jun, LI Xiangdong, PU Xuyang, et al. Calibration and evaluation of flow field in combustion-heating hypersonic high-temperature wind tunnels[J]. Journal of Propulsion Technology, 2022, 43(10): 210122. (in Chinese
WU Jun, LI Xiangdong, PU Xuyang, et al. Calibration and evaluation of flow field in combustion-heating hypersonic high-temperature wind tunnels[J]. Journal of Propulsion Technology, 2022, 43(10): 210122. (in Chinese)
|
| [4] |
LIU Qili, BACCARELLA D, LANDSBERG W, et al. Cavity flameholding in an optical axisymmetric scramjet in Mach 4.5 flows[J]. Proceedings of the Combustion Institute, 2019, 37(3): 3733-3740. doi: 10.1016/j.proci.2018.08.037
|
| [5] |
李俊红, 苗文博, 谌君谋, 等. 高温非平衡流地面试验及数值模拟[J]. 航空动力学报, 2023, 38(11): 2574-2582. LI Junhong, MIAO Wenbo, CHEN Junmou, et al. Ground test and numerical simulation on high temperature non-equilibrium flow[J]. Journal of Aerospace Power, 2023, 38(11): 2574-2582. (in Chinese
LI Junhong, MIAO Wenbo, CHEN Junmou, et al. Ground test and numerical simulation on high temperature non-equilibrium flow[J]. Journal of Aerospace Power, 2023, 38(11): 2574-2582. (in Chinese)
|
| [6] |
卢洪波, 陈星, 谌君谋, 等. 新建高焓激波风洞Ma=8飞行模拟条件的实现与超燃实验[J]. 气体物理, 2019, 4(5): 13-24. LU Hongbo, CHEN Xing, CHEN Junmou, et al. Flight condition achievement of Mach number 8 in a new shock tunnel of CAAA and its scramjet experimental investigation[J]. Physics of Gases, 2019, 4(5): 13-24. (in Chinese
LU Hongbo, CHEN Xing, CHEN Junmou, et al. Flight condition achievement of Mach number 8 in a new shock tunnel of CAAA and its scramjet experimental investigation[J]. Physics of Gases, 2019, 4(5): 13-24. (in Chinese)
|
| [7] |
张小庆, 吕金洲, 刘伟雄, 等. 脉冲风洞一体化飞行器测力精度分析[J]. 航空动力学报, 2018, 33(12): 2924-2929. ZHANG Xiaoqing, LYU Jinzhou, LIU Weixiong, et al. Analysis on the force measurement accuracy of the integrated vehicle in the impulse wind tunnel[J]. Journal of Aerospace Power, 2018, 33(12): 2924-2929. (in Chinese
ZHANG Xiaoqing, LYU Jinzhou, LIU Weixiong, et al. Analysis on the force measurement accuracy of the integrated vehicle in the impulse wind tunnel[J]. Journal of Aerospace Power, 2018, 33(12): 2924-2929. (in Chinese)
|
| [8] |
赵荣娟, 刘施然, 周正, 等. 激波风洞超燃冲压发动机推力测量技术研究[J]. 实验流体力学, 2022, 36(4): 103-108. ZHAO Rongjuan, LIU Shiran, ZHOU Zheng, et al. Research of scramjet thrust test in shock tunnel[J]. Journal of Experiments in Fluid Mechanics, 2022, 36(4): 103-108. (in Chinese
ZHAO Rongjuan, LIU Shiran, ZHOU Zheng, et al. Research of scramjet thrust test in shock tunnel[J]. Journal of Experiments in Fluid Mechanics, 2022, 36(4): 103-108. (in Chinese)
|
| [9] |
HOLDEN M S, TIMOTHY P W, MATTHEW M, et al. Experimental research and analysis in supersonic and hypervelocity flows in the LENS shock tunnels and expansion tunnel[R]. AIAA-2015-3660, 2015.
|
| [10] |
林键, 卢洪波, 王瑞庭, 等. FD-21风洞冲压发动机Ma10流场与乙烯燃烧建立过程[J]. 力学学报, 2023, 55(8): 1788-1799. LIN Jian, LU Hongbo, WANG Ruiting, et al. Establishing process of scramjet flow and ethylene-burning at Ma10 conditions of FD-21 shock tunnel[J]. Chinese Journal of Theoretical and Applied Mechanics, 2023, 55(8): 1788-1799. (in Chinese
LIN Jian, LU Hongbo, WANG Ruiting, et al. Establishing process of scramjet flow and ethylene-burning at Ma10 conditions of FD-21 shock tunnel[J]. Chinese Journal of Theoretical and Applied Mechanics, 2023, 55(8): 1788-1799. (in Chinese)
|
| [11] |
MOURA A F, GIBBONS N, WHEATLEY V, et al. Characterization of supersonic turbulent combustion in a Mach-10 scramjet combustor[J]. AIAA Journal, 2020, 58(5): 2180-2196. doi: 10.2514/1.J058671
|
| [12] |
OBYRNE S, DANEHY P M, CUTLER A D, et al. Dual-pump CARS thermometry and species concentration measurements in a supersonic combustor[R]. AIAA-2004-0710, 2004.
|
| [13] |
ZHOU Gongxi, ZHANG Xu, LI Jinping, et al. Optical diagnostics in a detonation-driven direct-connected circular combustor fueled with hydrogen for Mach 10 scramjet[J]. International Journal of Hydrogen Energy, 2021, 46(54): 27801-27815. doi: 10.1016/j.ijhydene.2021.06.004
|
| [14] |
王林森, 涂晓波, 王宇航, 等. 基于acetone-PLIF技术的超燃冲压发动机燃烧室燃料/空气掺混特性[J]. 航空动力学报, 2021, 36(8): 1614-1620. WANG Linsen, TU Xiaobo, WANG Yuhang, et al. Fuel/air mixing characteristics of scramjet combustor based on acetone-PLIF technology[J]. Journal of Aerospace Power, 2021, 36(8): 1614-1620. (in Chinese
WANG Linsen, TU Xiaobo, WANG Yuhang, et al. Fuel/air mixing characteristics of scramjet combustor based on acetone-PLIF technology[J]. Journal of Aerospace Power, 2021, 36(8): 1614-1620. (in Chinese)
|
| [15] |
袁勋, 于欣, 彭江波, 等. 电弧风洞NO平面激光诱导荧光可视化方法与试验验证[J]. 航空学报, 2023, 44(19): 128391. YUAN Xun, YU Xin, PENG Jiangbo, et al. Research and experimental verification of NO-PLIF visualization method in arc-heated wind tunnel[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(19): 128391. (in Chinese
YUAN Xun, YU Xin, PENG Jiangbo, et al. Research and experimental verification of NO-PLIF visualization method in arc-heated wind tunnel[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(19): 128391. (in Chinese)
|
| [16] |
吴戈, 李韵, 万明罡, 等. 平面激光诱导荧光技术在超声速燃烧火焰结构可视化中的应用[J]. 实验流体力学, 2020, 34(3): 70-77. WU Ge, LI Yun, WAN Minggang, et al. Visualization of flame structure in supersonic combustion by Planar Laser Induced Fluorescence technique[J]. Journal of Experiments in Fluid Mechanics, 2020, 34(3): 70-77. (in Chinese
WU Ge, LI Yun, WAN Minggang, et al. Visualization of flame structure in supersonic combustion by Planar Laser Induced Fluorescence technique[J]. Journal of Experiments in Fluid Mechanics, 2020, 34(3): 70-77. (in Chinese)
|
| [17] |
VANYAI T, LANDSBERG W O, MCINTYRE T J, et al. OH visualization of ethylene combustion modes in the exhaust of a fundamental, supersonic combustor[J]. Combustion and Flame, 2021, 226: 143-155.
|
| [18] |
JEONG E, O’BYRNE S, JEUNG I S, et al. The effect of fuel injection location on supersonic hydrogen combustion in a cavity: based model scramjet combustor[R]. Energies, 2020, 13(1): 193.
|
| [19] |
VANYAI T, GRIEVE S, STREET O, et al. Fundamental scramjet combustion experiments using hydrocarbon fuel[J]. Journal of Propulsion and Power, 2019, 35(5): 953-963.
|
| [20] |
武国华, 于欣, 彭江波, 等. 超燃冲压发动机羟基/煤油-PLIF同步测量研究[J]. 推进技术, 2024, 45(1): 2210098. WU Guohua, YU Xin, PENG Jiangbo, et al. Simultaneous measurements of OH/kerosene-PLIF in scramjet[J]. Journal of Propulsion Technology, 2024, 45(1): 2210098. (in Chinese
WU Guohua, YU Xin, PENG Jiangbo, et al. Simultaneous measurements of OH/kerosene-PLIF in scramjet[J]. Journal of Propulsion Technology, 2024, 45(1): 2210098. (in Chinese)
|
| [21] |
曹振, 于欣, 彭江波, 等. 用于大尺度模型发动机高频PLIF测量的脉冲串紫外激光系统[J]. 光谱学与光谱分析, 2024, 44(4): 932-936. CAO Zhen, YU Xin, PENG Jiangbo, et al. A burst-mode ultraviolet laser system for high-speed PLIF measurements in large-scale model engine[J]. Spectroscopy and Spectral Analysis, 2024, 44(4): 932-936. (in Chinese
CAO Zhen, YU Xin, PENG Jiangbo, et al. A burst-mode ultraviolet laser system for high-speed PLIF measurements in large-scale model engine[J]. Spectroscopy and Spectral Analysis, 2024, 44(4): 932-936. (in Chinese)
|
| [22] |
高龙, 于欣, 彭江波, 等. 超燃冲压发动机点火过程10 kHz PLIF测量技术[J]. 推进技术, 2022, 43(12): 210739. GAO Long, YU Xin, PENG Jiangbo, et al. 10 kHz PLIF measurement technique for scramjet ignition[J]. Journal of Propulsion Technology, 2022, 43(12): 210739. (in Chinese
GAO Long, YU Xin, PENG Jiangbo, et al. 10 kHz PLIF measurement technique for scramjet ignition[J]. Journal of Propulsion Technology, 2022, 43(12): 210739. (in Chinese)
|
| [23] |
SOPEK T, BRIESCHENK S, VANYAI T, et al. Iron contamination in high-enthalpy test facilities: OH PLIF imaging considerations[J]. Journal of Propulsion and Power, 2019, 36(1): 129-137.
|
DownLoad:
