Volume 41 Issue 4
Apr.  2026
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ZHANG Zehao, DONG Libao, ZHAO Liyou, et al. Numerical simulation of acoustic mode characteristics of combustion chamber considering influence of dome[J]. Journal of Aerospace Power, 2026, 41(4):20250119 doi: 10.13224/j.cnki.jasp.20250119
Citation: ZHANG Zehao, DONG Libao, ZHAO Liyou, et al. Numerical simulation of acoustic mode characteristics of combustion chamber considering influence of dome[J]. Journal of Aerospace Power, 2026, 41(4):20250119 doi: 10.13224/j.cnki.jasp.20250119

Numerical simulation of acoustic mode characteristics of combustion chamber considering influence of dome

doi: 10.13224/j.cnki.jasp.20250119
  • Received Date: 2025-03-10
    Available Online: 2025-06-28
  • Numerical simulation of the acoustic mode characteristics of the combustion chamber with the dome was carried out based on the coupled computational aeroacoustic (CAA)/low-order thermoacoustic network method. The eigenfrequencies, damping rates and acoustic pressure distribution clouds of the main acoustic modes of the combustion chamber were obtained, the accuracy and efficiency of the coupling methods were verified, and the influence of the dome on the acoustic mode characteristics was compared and analyzed. The results showed that, after considering the influence of the dome which was coupled with the acoustic pressure distribution of the combustion chamber, the damping rate of the first-order transverse and longitudinal modes of the combustion chamber was reduced by 24.5% and 16%, but the effect on eigenfrequency was not obvious; compared with the CAA method, the coupling method can improve the calculation efficiency by 49% under the condition of ensuring the calculation accuracy, making it very suitable for the engineering of multi-nozzle liquid rocket engine combustion chamber.

     

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  • [1]
    汪广旭, 李斌, 谭永华, 等. 液体火箭发动机高频燃烧不稳定问题综述[J]. 航空学报, 2024, 45(11): 529450. WANG Guangxu, LI Bin, TAN Yonghua, et al. High frequency combustion instability in liquid rocket engines: Review[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(11): 529450. (in Chinese

    WANG Guangxu, LI Bin, TAN Yonghua, et al. High frequency combustion instability in liquid rocket engines: Review[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(11): 529450. (in Chinese)
    [2]
    聂万胜, 庄逢辰, 张中光. 液体火箭发动机中声腔抑制不稳定燃烧的声学分析[J]. 应用声学, 2001, 20(4): 35-39. NIE Wansheng, ZHUANG Fengchen, ZHANG Zhongguang. Acoustic analysis of resonators for combustion instability suppression in liquid rocket engines[J]. Applied Acoustics, 2001, 20(4): 35-39. (in Chinese doi: 10.3969/j.issn.1000-310X.2001.04.007

    NIE Wansheng, ZHUANG Fengchen, ZHANG Zhongguang. Acoustic analysis of resonators for combustion instability suppression in liquid rocket engines[J]. Applied Acoustics, 2001, 20(4): 35-39. (in Chinese) doi: 10.3969/j.issn.1000-310X.2001.04.007
    [3]
    覃建秀, 张会强, 王兵. 基于数值定容弹方法的燃烧室声学特性研究[J]. 推进技术, 2018, 39(2): 366-373. QIN Jianxiu, ZHANG Huiqiang, WANG Bing. Investigation on acoustic characteristic of thruster with numerical constant-volume bomb method[J]. Journal of Propulsion Technology, 2018, 39(2): 366-373. (in Chinese

    QIN Jianxiu, ZHANG Huiqiang, WANG Bing. Investigation on acoustic characteristic of thruster with numerical constant-volume bomb method[J]. Journal of Propulsion Technology, 2018, 39(2): 366-373. (in Chinese)
    [4]
    杨 V, 安德松W E. 液体火箭发动机燃烧不稳定性[M]. 张宝炯, 洪鑫, 陈杰, 译. 北京: 科学出版社, 2001. YANG V, ANDERSON W E. Liquid rocket engine combustion instability[M]. Translated by ZHANG Baojiong, HONG Xin, CHEN Jie. Beijing: Science Press, 2001. (in Chinese

    YANG V, ANDERSON W E. Liquid rocket engine combustion instability[M]. Translated by ZHANG Baojiong, HONG Xin, CHEN Jie. Beijing: Science Press, 2001. (in Chinese)
    [5]
    付虓, 郭志辉, 杨甫江. 模型预混燃烧室线性稳定性分析[J]. 航空动力学报, 2015, 30(5): 1099-1105. FU Xiao, GUO Zhihui, YANG Fujiang. Linear stability analysis of modal premixed combustor[J]. Journal of Aerospace Power, 2015, 30(5): 1099-1105. (in Chinese

    FU Xiao, GUO Zhihui, YANG Fujiang. Linear stability analysis of modal premixed combustor[J]. Journal of Aerospace Power, 2015, 30(5): 1099-1105. (in Chinese)
    [6]
    曹晨, 谭永华, 陈建华, 等. 气喷嘴和声腔对燃烧室声学特性的影响[J]. 航空动力学报, 2019, 34(8): 1836-1846. CAO Chen, TAN Yonghua, CHEN Jianhua, et al. Effects of gas nozzle and resonators on acoustic characteristics of combustion chamber[J]. Journal of Aerospace Power, 2019, 34(8): 1836-1846. (in Chinese

    CAO Chen, TAN Yonghua, CHEN Jianhua, et al. Effects of gas nozzle and resonators on acoustic characteristics of combustion chamber[J]. Journal of Aerospace Power, 2019, 34(8): 1836-1846. (in Chinese)
    [7]
    曹晨, 谭永华, 陈建华, 等. 大直径液氧煤油发动机燃烧室结构和隔板型式对声学特性的影响[J]. 推进技术, 2021, 42(7): 1581-1592. CAO Chen, TAN Yonghua, CHEN Jianhua, et al. Influence of combustion chamber structure and baffle type on acoustic characteristics of large diameter liquid oxygen kerosene engine[J]. Journal of Propulsion Technology, 2021, 42(7): 1581-1592. (in Chinese

    CAO Chen, TAN Yonghua, CHEN Jianhua, et al. Influence of combustion chamber structure and baffle type on acoustic characteristics of large diameter liquid oxygen kerosene engine[J]. Journal of Propulsion Technology, 2021, 42(7): 1581-1592. (in Chinese)
    [8]
    初敏, 徐旭. 高频不稳定燃烧的声学数值仿真[J]. 北京航空航天大学学报, 2015, 41(7): 1215-1222. CHU Min, XU Xu. Acoustic numerical simulation of high frequency combustion instability[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(7): 1215-1222. (in Chinese

    CHU Min, XU Xu. Acoustic numerical simulation of high frequency combustion instability[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(7): 1215-1222. (in Chinese)
    [9]
    GUO Kangkang, NIE Wansheng, LIU Yu, et al. Numerical simulation of damping capacity between injector-formed baffle and normal blade baffle in a kero/LOX liquid rocket engine[C]//Proceedings of the Advances in Materials, Machinery, Electrical Engineering (AMMEE 2017). Dordrecht, Netherlands: Atlantis Press, 2017: 559-568.
    [10]
    王枫, 李龙飞, 张贵田. 液氧煤油补燃发动机喷注器高频燃烧不稳定性的试验研究[J]. 宇航学报, 2012, 33(2): 260-264. WANG Feng, LI Longfei, ZHANG Guitian. Experimental study on high frequency combustion instability with coaxial injector of staged combustion LOX/kerosene rocket engine[J]. Journal of Astronautics, 2012, 33(2): 260-264. (in Chinese

    WANG Feng, LI Longfei, ZHANG Guitian. Experimental study on high frequency combustion instability with coaxial injector of staged combustion LOX/kerosene rocket engine[J]. Journal of Astronautics, 2012, 33(2): 260-264. (in Chinese)
    [11]
    LIOI C, KU D, YANG V. Linear acoustic analysis of main combustion chamber of an oxidizer-rich staged combustion engine[J]. Journal of Propulsion and Power, 2018, 34(6): 1505-1518. doi: 10.2514/1.B36878
    [12]
    HEILMANN G, HIRSCH C, SATTELMAYER T. Energetically consistent computation of combustor stability with a model consisting of a helmholtz-fem-domain and a Low-Order Network[J]. Journal of Engineering for Gas Turbines Power, 2021, 143(5).
    [13]
    NI F, NICOUD F, MÉRY Y, et al. Including flow-acoustic interactions in the Helmholtz computations of industrial combustors[J]. AIAA Journal, 2018, 56(12): 4815-4829. doi: 10.2514/1.J057093
    [14]
    LAERA D, CAMPA G, CAMPOREALE S M, et al. Modelling of thermoacoustic combustion instabilities phenomena: application to an experimental test rig[J]. Energy Procedia, 2014, 45(3): 1392-1401.
    [15]
    CAMPA G, CAMPOREALE S M. Eigenmode analysis of the thermoacoustic combustion instabilities using a hybrid technique based on the finite element method and the transfer matrix method[J]. Advances in Applied Acoustics, 2012, 1(1): 1-14.
    [16]
    CAMPA G, CAMPOREALE S M. Prediction of the thermoacoustic combustion instabilities in practical annular combustors[J]. Journal of Engineering for Gas Turbines and Power, 2014, 136(9): 091504. doi: 10.1115/1.4027067
    [17]
    SCHULZE M, SATTELMAYER T. A comparison of time and frequency domain descriptions of high frequency acoustics in rocket engines with focus on dome coupling[J]. Aerospace Science and Technology, 2015, 45(9): 165-173.
    [18]
    SCHULZE M. Linear stability assessment of cryogenic rocket engines [D]. Munich, Germany: Technische Universitaet Muenchen, 2016.
    [19]
    张贵田. 高压补燃液氧煤油发动机[M]. 北京: 国防工业出版社, 2005. ZHANG Guitian. High pressure staged combustion LOX/Kerosene rocket engine[M]. Beijing: National Defense Industry Press, 2005. (in Chinese

    ZHANG Guitian. High pressure staged combustion LOX/Kerosene rocket engine[M]. Beijing: National Defense Industry Press, 2005. (in Chinese)
    [20]
    FISCHER A, HIRSCH C, SATTELMAYER T. Comparison of multi-microphone transfer matrix measurements with acoustic network models of swirl burners[J]. Journal of Sound and Vibration, 2006, 298(1/2): 73-83.
    [21]
    SATTELMAYER T, KATHAN R, KOEGLMEIER S. Validation of transverse instability damping computations for rocket engines[J]. Journal of Propulsion and Power, 2015, 31(4): 1-11.
    [22]
    SMITH R J. Computational investigations of high frequency acoustics and instabilities in a single-element rocket combustor [D]. West Lafayette, US: Purdue University, 2010.
    [23]
    张泽昊, 樊志伟, 董立宝, 等. 隔板对液体火箭发动机燃烧室声学模态特性的影响[J]. 航空动力学报, 2024, 39(4): 20220352. ZHANG Zehao, FAN Zhiwei, DONG Libao, et al. Effects of baffle on the acoustic mode characteristics of liquid rocket engine combustion chambers[J]. Journal of Aerospace Power, 2024, 39(4): 20220352. (in Chinese

    ZHANG Zehao, FAN Zhiwei, DONG Libao, et al. Effects of baffle on the acoustic mode characteristics of liquid rocket engine combustion chambers[J]. Journal of Aerospace Power, 2024, 39(4): 20220352. (in Chinese)
    [24]
    HARVAZINSKI M E, GEJJI R M, Talley D G, et al. Modeling of transverse combustion instability[C]//Proceedings of the AIAA SciTech forum. Reston, US: American Institute of Aeronautics and Astronautics, 2019: 1732.
    [25]
    ORTH M R, VODNEY C, LIU T, et al. Measurement of linear growth of self-excited instabilities in an idealized rocket combustor[C]//Proceedings of the AIAA Aerospace Sciences Meeting. Kissimmee, US: American Institute of Aeronautics and Astronautics, 2018: 1185.
    [26]
    GEJJI R, LEMCHERFI A I, STRELAU R, et al. Combustion response of shear coaxial injectors to transverse combustion instabilities[C]//Proceedings of the AIAA SciTech forum. Orlando, US: American Institute of Aeronautics and Astronautics, 2020: 0424.
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