Numerical Simulation of Quenched Combustion Model for AP/HTPB Propellant under Transient Depressurization

被引:15
|
作者
Ye, Zhen-Wei [1 ]
Yu, Yong-Gang [1 ]
机构
[1] Nanjing Univ Sci & Technol, Sch Energy & Power Engn, Nanjing 210094, Jiangsu, Peoples R China
关键词
AP; HTPB; composite solid propellant; out-of-phase blowing effect; unsteady combustion; COMPOSITE PROPELLANTS; FLAME STRUCTURE; SANDWICHES;
D O I
10.1002/prep.201700017
中图分类号
O69 [应用化学];
学科分类号
081704 ;
摘要
In order to study the out-of-phase blowing effect of ammonium perchlorate/hydroxyl terminated polybutadiene (AP/HTPB) under transient depressurization, a two-dimensional periodic sandwich model of AP/HTPB sandwich unsteady combustion was established. The gas-solid two-step total reaction was used to couple the gas-solid boundary layer, and the AP/HTPB step-down temperature criterion was applied. The numerical simulation comparative analysis under the initial combustion pressure 3.5MPa approximate to 10MPa and the initial depressurization rate of 1000MPa/s approximate to 2000MPa/s was experimented. The results show that under the condition of initial combustion pressure of 3.5MPa and pressure reduction rate of 1000MPa/s, the formation of narrow diffusion chemical reaction zone appears in the initial stage of depressurization; when the combustion pressure drops to about 1.7MPa, the flame appears dual characteristics: diffusion and premixed combustion; when the pressure dropped to 0.1MPa, the flame is premixed combustion. AP(g) is the main factor causing the out-of-phase blowing effect. During the initial stage of combustion, AP(g) decomposes rapidly and its decomposition product is close to the combustion surface; with the rapid decrease of pressure, the gas-phase heat feedback decreases, leading to the decrease of AP(g) decomposition rate and AP(g) diffusion to the gas phase, which is the initial phase of out-of-phase blowing effect; when the gas phase heat feedback reduced and the temperature is below 750K, the decomposition of AP(g) is stopped and the undecomposed AP(g) is further diffused to the gas phase region, which exacerbates the out-of-phase blowing effect, leading to the extinguishment of AP/HTPB. The unsteady combustion flame extinction time increases with the initial combustion pressure, and decreases with the initial depressurization rate.
引用
收藏
页码:1085 / 1094
页数:10
相关论文
共 50 条
  • [21] Investigation on the microscale combustion characteristics of AP/HTPB propellant under wide pressure range
    Zou, Xiangrui
    Wang, Ningfei
    Wang, Chao
    Wang, Junlong
    Tang, Yong
    Shi, Baolu
    FUEL, 2021, 306
  • [22] AP-HTPB propellant combustion under strain conditions with laser absorption spectroscopy
    Gu, Mingming
    Ouyang, Jianfeng
    Wang, Shaojie
    Yuan, Wenhao
    Shi, Xiaoming
    Hou, Kaiyu
    Xiao, Libai
    Gao, Hongxu
    Zhou, Zhongyue
    Qi, Fei
    APPLIED OPTICS, 2023, 62 (06) : A37 - A45
  • [23] Thermal decomposition and combustion characteristics of Al/AP/HTPB propellant
    Yuan, Jifei
    Liu, Jianzhong
    Zhou, Yunan
    Zhang, Yanwei
    Cen, Kefa
    JOURNAL OF THERMAL ANALYSIS AND CALORIMETRY, 2021, 143 (06) : 3935 - 3944
  • [24] Ignition and combustion characteristics of AP/HTPB composite propellant by laser
    Zhang, Lingke
    Zhao, Wei
    Wu, Lizhi
    Zhongguo Jiguang/Chinese Journal of Lasers, 2013, 40 (08):
  • [25] Thermal decomposition and combustion characteristics of Al/AP/HTPB propellant
    Jifei Yuan
    Jianzhong Liu
    Yunan Zhou
    Yanwei Zhang
    Kefa Cen
    Journal of Thermal Analysis and Calorimetry, 2021, 143 : 3935 - 3944
  • [26] Effects of AP powder topology on microscale combustion properties of AP/HTPB propellant
    Zou, Xiangrui
    Wang, Ningfei
    Chen, Yi
    Han, Lei
    Wang, Junlong
    Wang, Chao
    Shi, Baolu
    POWDER TECHNOLOGY, 2021, 394 : 468 - 477
  • [27] 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
  • [28] Numerical study on the effect of pressure on transient micro-combustion and heat release characteristics of AP/HTPB/Al composite propellant fuel
    Liu, Shuyuan
    He, Pengxiang
    Han, Luyang
    Ding, Yanyu
    Wang, Limin
    Han, Jinchao
    Hu, Songqi
    FUEL, 2023, 347
  • [29] Numerical Simulation of the Pouring Process of HTPB Propellant
    Jiang X.-R.
    Li Z.
    Lu R.
    Huang D.-H.
    Hanneng Cailiao/Chinese Journal of Energetic Materials, 2020, 28 (08): : 724 - 730
  • [30] Heat transfer process and reaction mechanism of AP/HTPB propellant under transient high temperature
    Zhang, Yixiao
    Zhang, Qi
    INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2024, 219