Numerical Analysis of Thermal Response of UHTCs under Aerodynamic Heating

被引：0
|
作者：
Liu, Miaoqun [1 ]
Lv, Hongqing [1 ]
Wang, Zhenqing [1 ]
机构：
[1] Harbin Engn Univ, Coll Aerosp & Civil Engn, Harbin 150001, Peoples R China
来源：
MECHATRONICS AND INTELLIGENT MATERIALS II, PTS 1-6 | 2012年 / 490-495卷
关键词：
Numerical analysis; Aerodynamic heating; Ultrahigh temperature ceramics(UHTCs); Thermal response;
D O I：
10.4028/www.scientific.net/AMR.490-495.2314
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
Based on the theory and semi-empirical formulas, the surface heating flux of hypersonic flying vehicle under aerodynamic heating is calculated by using reference enthalpy method. On this basis, the thermal response of structure made of ultrahigh temperature ceramics(UHTCs) is simulated by using finite-element method. The results show that thermal stress shock is able to cause material to damage in a very short time.
引用
收藏
页码：2314 / 2317
页数：4
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