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作 者:罗中一 杨自春[1] 费志方 LUO Zhongyi;YANG Zichun;FEI Zhifang(College of Power Engineering,Naval University of Engineering,Wuhan 430033,Chin)
出 处:《航空动力学报》2018年第6期1363-1369,共7页Journal of Aerospace Power
基 金:国家部委基金资助项目(9140A27030514JB11449)
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、1 200K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。A noncrystalline silica model and a primary particle model was built based on the theory of molecular dynamic and the algorithm of its simulation,and it explored how the solid phase thermal conductivity of aerogel was affected by the changes of external environmental conditions and aerogel internal structure.The results of silica aerogel solid phase thermal conductivity under four different enviromental temperatures,namely,300,500,800 Kand 1 200 K were obtained.With the enviromental temperature rise the solid phase thermal conductivity increased slightly.The influence of the internal defect of primary particle on the solid phase thermal conductivity of skeleton was discussed.Within the range of porosity,the thermal conductivity of the solid phase decreased with the increase of the porosity.When the porosity increased gradually to 0.26,the model can well characterize the actual situation.The noncrystalline aerogel model and algorithm proposed will provide a reference for the microscale heat transfer analysis and structural design of this material.
关 键 词:二氧化硅气凝胶 固相热导率 绝热材料 分子动力学 微尺度传热
分 类 号:V25[一般工业技术—材料科学与工程] TB34[航空宇航科学与技术—航空宇航制造工程]
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