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气凝胶骨架固相热导率的分子动力学模拟

罗中一 杨自春 费志方

罗中一, 杨自春, 费志方. 气凝胶骨架固相热导率的分子动力学模拟[J]. 航空动力学报, 2018, 33(6): 1363-1369. doi: 10.13224/j.cnki.jasp.2018.06.010
引用本文: 罗中一, 杨自春, 费志方. 气凝胶骨架固相热导率的分子动力学模拟[J]. 航空动力学报, 2018, 33(6): 1363-1369. doi: 10.13224/j.cnki.jasp.2018.06.010
Aerogel skeleton solid phase thermal conductivity by molecular dynamics simulation[J]. Journal of Aerospace Power, 2018, 33(6): 1363-1369. doi: 10.13224/j.cnki.jasp.2018.06.010
Citation: Aerogel skeleton solid phase thermal conductivity by molecular dynamics simulation[J]. Journal of Aerospace Power, 2018, 33(6): 1363-1369. doi: 10.13224/j.cnki.jasp.2018.06.010

气凝胶骨架固相热导率的分子动力学模拟

doi: 10.13224/j.cnki.jasp.2018.06.010
基金项目: 国家部委基金资助项目(9140A27030514JB11449)

Aerogel skeleton solid phase thermal conductivity by molecular dynamics simulation

  • 摘要: 基于分子动力学理论和模拟的算法,构建了非晶态二氧化硅模型以及初级粒子模型,研究了外界环境条件和气凝胶内部结构的变化对气凝胶固相热导率的影响规律。得到了300、500、800、1200K四种环境温度下二氧化硅气凝胶材料的固相热导率,材料的固相热导率随着环境温度上升略有增加。同时探讨了初级粒子内部缺陷对骨架固相热导率的影响,一定孔隙率范围内,随着孔隙率的增加材料的固相热导率降低,当孔隙率逐渐增加至0.26后,模型能够很好地表征实际情况。所建立的非晶态气凝胶模型及算法对该类材料的微尺度传热分析及结构设计具有借鉴价值。

     

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出版历程
  • 收稿日期:  2016-11-16
  • 刊出日期:  2018-06-28

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