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三维颗粒增强复合材料细观温度场计算
引用本文:孙志刚,宋迎东,高希光,苗艳.三维颗粒增强复合材料细观温度场计算[J].航空动力学报,2009,24(10):2285-2290.
作者姓名:孙志刚  宋迎东  高希光  苗艳
作者单位:南京航空航天大学能源与动力学院, 南京 210016
基金项目:高等学校博士学科点专项科研基金 
摘    要:将高阶理论推广到三维情况,采用界面平均温度代替温度函数中待定系数作为未知量,并取消了亚子胞的概念,减少了求解方程数量,有效地提高了计算效率.在单胞的热分析过程中,利用热流与平均温度之间的关系建立子胞热传导方程,进行温度场求解,并与有限元法计算结果进行了比较,验证了该方法的正确性和有效性. 

关 键 词:高阶理论    复合材料    细观结构    温度场
收稿时间:8/2/2008 6:44:07 PM
修稿时间:8/19/2009 3:20:58 PM

Temperature fields calculation of 3-D particle reinforced composite
SUN Zhi-gang,SONG Ying-dong,GAO Xi-guang and MIAO Yan.Temperature fields calculation of 3-D particle reinforced composite[J].Journal of Aerospace Power,2009,24(10):2285-2290.
Authors:SUN Zhi-gang  SONG Ying-dong  GAO Xi-guang and MIAO Yan
Institution:College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Abstract:The Higher-order theoty was developed to three-dimension, coefficients of temperature function were replaced by surface-averaged temperature to be primary variables of equations, and the concept of sub-cells was canceled. The number of equations was reduced so that computational efficiency was increased effectively. During the thermal analysis of represent volume element, heat exchange quations which established the relationship of hear flux and average temperature were used to compute temperature, The comparison of numerical results with finite element analysis demonstrated the correctively and validity.
Keywords:aerospace propulsion system  higher-order theory  composite  micro-structure  temperature fields
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