A bulk ablation model considering insulator expansion phenomenon
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    Abstract:

    According to the experimental phenomenon that carbon layer thickness is greater than the insulator matrix loss thickness, a bulk ablation model considering insulator expansion phenomenon with double regions is established. It's believed that expansion is produced during pyrolysis process and the formation rate of carbon layer is 2 times faster than the lapse rate of matrix. At each time step, the interface position of carbon layer and the matrix is determined according to the relationship between local temperature and insulator pyrolysis temperature, and the method of remeshing and data exchange coupling calculation are developed at the same time. The ablation rate and carbon layer porous structure obtained by the double regions bulk ablation model agree well with the experimental results, which proves that the model can basically describe the ablation details of EPDM(ethylene-propylene-diene monomer) insulator.

    Reference
    [1] 王书贤,何国强,李江,等.单纯热化学烧蚀环境下EPDM绝热材料炭化层结构特征分析[J].固体火箭技术,2010,33(2):214-117. WANG Shuxian, HE Guoqiang, LI Jiang, et al. Carburization layer structure character of EPDM insulator in simplex thermo-chemical ablation environment[J].Journal of Solid Rocket Technology, 2010,33(2):214-217.(in Chinese)
    [2] 王书贤,何国强,刘佩进,等.气相燃气速度对EPDM绝热材料烧蚀的影响[J].推进技术,2010,31(2):235-239. WANG Shuxian, HE Guoqiang, LIU Peijin, et al. The influence of gas-phase speed on EPDM insulator ablation[J].Journal of Propulsion Technology, 2010,31(2):235-239.(in Chinese)
    [3] Yang B C, Cheung F B, Koo J H. Numercal investigation of thermo-chemical and mechanical erosion of ablative materials[R].[S.l.]:AIAA,93-2045.
    [4] Yu I D. Effect of thermo mechanical erosion of heterogeneous combustion of composite materials in high-speed Flows[J].Combustion and Flame, 2000,122:211-226.
    [5] 李强,杨飒,李江,等.EPDM绝热材料耦合烧蚀模型[J].固体火箭技术,2012,35(1):114-117. LI Qiang, YANG Sa, LI Jiang, et al. Coupled ablation model for EPDM insulator[J].Journal of Solid Rocket Technology, 2012,35(1):114-117.(in Chinese)
    [6] Reynolds R A, Russell G W, Nourse R W. Ablation performance characterization of thermal protection material using a mach 4.4 sled test[R].[S.l.]:AIAA,92-3055.
    [7] Koo J H. Thermal characteristics comparison of two fire resistant materials[J].Journal of Fire Sciences, 1997,15:1027-1032.
    [8] Russell G W. Analytic modeling and experimental validation of intumescent behavior of charring heat shield materials[D].Huntsville, Alabama:The University of Alabama in Huntsville, 2002.
    [9] Clark R K. An analysis of a charring ablator with thermal nonequilibrium chemical kinetics and mass transfer[R].[S.l.]:NASA-TN-D-7180,June,1973.
    [10] Ayasoufi A, Rahmani R K, Cheng G, et al. Numerical simulation of ablation for reentry vehicles[R].[S.l.]:AIAA,2006-2908.
    [11] William K, Michael C, Bernhard W. Convective heat and mass transfer[M].[S.l.]:McGraw-Hill Inc, 1993.
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王书贤,徐义华.考虑炭化绝热材料膨胀现象的体烧蚀模型[J].重庆大学学报,2018,41(5):44~51

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History
  • Received:December 15,2017
  • Online: May 23,2018
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