摘要
本文采用有限元法,分析和计算了有热解的再入烧蚀体的传热问题。计算方法和程序先用两个算例进行了考证,最后给出了沿真实弹道的计算结果。
The finite element analysis and calculation of heat transfer in ablating bodies are presented. The analysis and computer program have been tested by calculating two examples, then results of calculation along a real trajectory are shown.
出处
《空气动力学学报》
CSCD
北大核心
1991年第2期218-225,共8页
Acta Aerodynamica Sinica
关键词
烧蚀
传热
有限元法
航天器
ablation, heat transfer, finite element method.
