Characteristics of ethylene-air continuous rotating detonation in the cavity-based annular combustor

被引:15
|
作者
Fan, Weijie [1 ]
Liu, Shijie [1 ]
Zhong, Shenghui [2 ]
Peng, Haoyang [1 ]
Yuan, Xueqiang [1 ]
Liu, Weidong [1 ]
机构
[1] Natl Univ Def Technol, Coll Aerosp Sci & Engn, Sci & Technol Scramjet Lab, Changsha, Hunan, Peoples R China
[2] Beihang Hangzhou Innovat Inst Yuhang, Hangzhou 310023, Zhejiang, Peoples R China
基金
中国国家自然科学基金;
关键词
WAVE; HYDROGEN; MIXTURE; MULTIPLICITY; DEFLAGRATION; SIMULATIONS; INITIATION; ENGINE;
D O I
10.1063/5.0147069
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Characteristics of continuous rotating detonation (CRD) in a cavity-based annular combustor are studied through three-dimensional simulations, which are solved in OpenFOAM with a skeletal chemical kinetics mechanism. The results show that the continuous rotating detonation wave (CRDW) attaches to the outer wall and detaches from the inner wall in the cavity-based annular combustor. A high-temperature recirculation zone is found in the cavity with reactive intermediate species in the cavity-based annular combustor. The cavity is identified as a high-temperature ignition source, which provides heat and active intermediate radicals enhancing the detonability of the combustible gases in front of the CRDW. Consequently, the propagation performance, the propulsive performance, and the detonation combustion intensity are promoted in the cavity-based annular combustor. The propagation mode of the CRDW transforms from an unstable mode to a single-wave mode with the application of cavity. As the cavity deepens from 0 to 15 mm, the propagation velocity significantly increases from 923.21 to 1662.81 m/s and the fuel-based specific impulse increases from 941.91 to 1044.48 s as the cavity depth varies from 0 to 15 mm. Furthermore, the detonation-dominant combustion fraction remarkably improves from 27.21% to 62.29%.
引用
收藏
页数:15
相关论文
共 50 条
  • [41] Investigation on flame characteristics approaching thermal chocking in a cavity-based supersonic combustor
    Cai, Zun
    Li, Jianbin
    Wang, Taiyu
    Wang, Yanan
    Zhu, Jiajian
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2023, 237 (03) : 741 - 747
  • [42] Experimental study of near-blowoff characteristics in a cavity-based supersonic combustor
    Song, Xiliang
    Wang, Hongbo
    Sun, Mingbo
    Zhang, Yanxiang
    ACTA ASTRONAUTICA, 2018, 151 : 37 - 43
  • [43] Mixing and combustion characteristics in a cavity-based supersonic combustor with different injection schemes
    Song, Xiliang
    Wang, Hongbo
    Sun, Mingbo
    Cai, Zun
    Liu, Chaoyang
    Yu, Jiangfei
    ACTA ASTRONAUTICA, 2019, 159 : 584 - 592
  • [44] Effect of kerosene injection states on mixing and combustion characteristics in a cavity-based supersonic combustor
    Liu, Xu
    Li, Peibo
    Li, Fei
    Wang, Hongbo
    Sun, Mingbo
    Wang, Chao
    Yang, Yixin
    Xiong, Dapeng
    Wang, Yanan
    CHINESE JOURNAL OF AERONAUTICS, 2024, 37 (04) : 308 - 320
  • [45] Effect of kerosene injection states on mixing and combustion characteristics in a cavity-based supersonic combustor
    Xu LIU
    Peibo LI
    Fei LI
    Hongbo WANG
    Mingbo SUN
    Chao WANG
    Yixin YANG
    Dapeng XIONG
    Yanan WANG
    Chinese Journal of Aeronautics, 2024, 37 (04) : 308 - 320
  • [46] Experimental study of mode transition characteristics of a cavity-based scramjet combustor during acceleration
    Meng, Yu
    Gu, Hongbin
    Zhuang, Jingheng
    Sun, Wenming
    Gao, Zhanbiao
    Lian, Huan
    Yue, Lianjie
    Chang, Xinyu
    AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 93
  • [47] Rotating detonation wave mechanics through ethylene-air mixtures in hollow combustors, and implications to high frequency combustion instabilities
    Anand, Vijay
    George, Andrew St.
    de Luzan, Charles Farbos
    Gutmark, Ephraim
    EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2018, 92 : 314 - 325
  • [48] Effect of variation of temperature on the internal flow characteristics of a strut and cavity-based SCRAMJET combustor
    Namrata Bordoloi
    K. Vaishali
    C. Arunkumar
    P. Chanakyan
    undefined Ramkumar
    Interactions, 245 (1)
  • [49] Distribution characteristics and mixing mechanism of a liquid jet injected into a cavity-based supersonic combustor
    Li, Peibo
    Li, Chenyang
    Wang, Hongbo
    Sun, Mingbo
    Liu, Chaoyang
    Wang, Zhenguo
    Huang, Yuhui
    AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 94
  • [50] Continuous detonation combustion of ternary "hydrogen-liquid propane-air" mixture in annular combustor
    Frolov, S. M.
    Aksenov, V. S.
    Ivanov, V. S.
    Shamshin, I. O.
    INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2017, 42 (26) : 16808 - 16820