Investigation on Enhancement of AP/HTPB/Al Composite Solid Propellant Combustion Characteristics via DC Electric Field

被引:0
|
作者
Huang, Xing [1 ]
Gan, Yunhua [1 ]
Ao, Wen [2 ]
Chen, Ningguang [1 ]
Luo, Yanlai [1 ]
Jiang, Zhengwei [1 ]
机构
[1] South China Univ Technol, Sch Elect Power Engn, Wushan Rd, Guangzhou 510640, Peoples R China
[2] Northwestern Polytech Univ, Internal Flow & Thermostructure Lab, Sci & Technol Combust, Xian, Peoples R China
基金
中国国家自然科学基金;
关键词
Solid propellant; DC electric field; burning rates; sandwich model; combustion mechanism; ROCKET-MOTOR; COUPLED SIMULATION; IGNITION TRANSIENT; VARIABLE-THRUST; MODEL; ALUMINUM;
D O I
10.1080/00102202.2024.2393670
中图分类号
O414.1 [热力学];
学科分类号
摘要
To investigate the influence mechanisms of DC electric fields on the combustion of solid propellants, a numerical model for the combustion characteristics of AP/HTPB/Al composite solid propellant under the DC electric field is established. Effects of the applied electric field on combustion flame structure, combustion surface temperature distribution, and mixing fraction distribution are analyzed. The results indicate that the applied electric field enhances the mixing effect of the propellant gas phase decomposition products, thereby altering the flame structure and bringing it closer to the combustion surface. The application of the electric field leads to an increase in the combustion surface temperature by 20-70 K. The effect of the negative electric field on the combustion surface temperature and burning rate is more significant compared to that of the positive electric field. The results provide valuable theoretical guidance in the field of solid engine combustion control. [GRAPHICS]
引用
收藏
页数:20
相关论文
共 50 条
  • [31] Influence of tailored CuO and Al/CuO nanothermites on the thermocatalytic degradation of nitrocellulose and combustion performance of AP/HTPB composite propellant
    Ningning Zhao
    Haixia Ma
    Ergang Yao
    Zhong Yu
    Ting An
    Fengqi Zhao
    Xiaojiao Yu
    Cellulose, 2021, 28 : 8671 - 8691
  • [32] Estimation of surface geometry on combustion characteristics of AP/ HTPB propellant under rapid depressurization
    Chen, Kaixuan
    Ye, Zhenwei
    Xue, Xiaochun
    Yu, Yonggang
    DEFENCE TECHNOLOGY, 2024, 33 : 546 - 558
  • [33] Estimation of surface geometry on combustion characteristics of AP/HTPB propellant under rapid depressurization
    Kaixuan Chen
    Zhenwei Ye
    Xiaochun Xue
    Yonggang Yu
    Defence Technology, 2024, 33 (03) : 546 - 558
  • [34] Application of spherical ultrafine CuO@AP with core–shell in AP/HTPB composite solid propellant
    Jie Liu
    Haomiao Yu
    Deqi Wang
    Sensen Sun
    Fengsheng Li
    Journal of Thermal Analysis and Calorimetry, 2023, 148 : 5235 - 5246
  • [35] Experimental study of material behavior of AP-HTPB base composite solid propellant
    Shin-Hoe Kim
    Yong-Taek Im
    Journal of Mechanical Science and Technology, 2019, 33 : 3355 - 3361
  • [36] Experimental study of material behavior of AP-HTPB base composite solid propellant
    Kim, Shin-Hoe
    Im, Yong-Taek
    JOURNAL OF MECHANICAL SCIENCE AND TECHNOLOGY, 2019, 33 (07) : 3355 - 3361
  • [37] Cook-off test and numerical simulation of AP/HTPB composite solid propellant
    Yang, Hou-Wen
    Yu, Yong-Gang
    Ye, Rui
    Xue, Xiao-Chun
    Li, Wen-Feng
    JOURNAL OF LOSS PREVENTION IN THE PROCESS INDUSTRIES, 2016, 40 : 1 - 9
  • [38] Burning Characteristics and Thermochemical Behavior of AP/HTPB Composite Propellant Using Coarse and Fine AP Particles
    Kohga, Makoto
    PROPELLANTS EXPLOSIVES PYROTECHNICS, 2011, 36 (01) : 57 - 64
  • [39] NEW HTPB/AP/Al PROPELLANT COMBUSTION PROCESS IN THE PRESENCE OF ALUMINUM NANO-PARTICLES
    Trubert, Jean-Francois
    Hommel, Jean
    Lambert, Dominique
    Fabignon, Yves
    Orlandi, Olivier
    INTERNATIONAL JOURNAL OF ENERGETIC MATERIALS AND CHEMICAL PROPULSION, 2008, 7 (02) : 99 - 122
  • [40] Mechanical properties and burning characteristics of AP/HTPB composite propellant using polytetrahydrofuran as a plasticizer
    Kohga, Makoto
    SCIENCE AND TECHNOLOGY OF ENERGETIC MATERIALS, 2010, 71 (5-6) : 145 - 150