摘要
以相关地面模拟飞行考核试验条件为依据,对通用再入飞行器长时间大面积防隔热连接结构进行了三维模拟仿真,给出了计算的温升数据曲线,与试验结果吻合较好,对同类防隔热结构的设计和工艺的优化具有一定的理论指导意义。
According to the correlative flight simulation test condition,3D computer simulation calculation was completed for an integrated structure of thermal protection/insulation of common reentry vehicle and temperature rise values were obtained. The temperature rise value of computer simulation accorded well with the test result. This work can instruct the design and technics optimization for the same structure of thermal protection/insulation.
出处
《宇航材料工艺》
CAS
CSCD
北大核心
2009年第1期14-16,共3页
Aerospace Materials & Technology
关键词
防隔热
一体化
结构
计算
模拟
Thermal protection/insulation, Integrated, Structure, Calculation, Simulation
