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作 者:孙志刚[1] 宋迎东[1] 高希光[1] 苗艳[1]
机构地区:[1]南京航空航天大学能源与动力学院,南京210016
出 处:《航空动力学报》2009年第10期2285-2290,共6页Journal of Aerospace Power
基 金:高校博士点基金(20070287039)
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.The higher-order theory 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 equations which were established by the relationship between hear flux and average temperature were used to compute temperature,...
分 类 号:TB33[一般工业技术—材料科学与工程]
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