Modeling of the radiation properties of flow around the hypersonic aircrafts

被引:1
作者
Zhao Yang-sheng [1 ]
Du Xiao-ping [2 ]
机构
[1] Acad Equipment, Dept Space Equipment, Beijing 101416, Peoples R China
[2] Acad Equipment, Dept Space & Command, Beijing 101416, Peoples R China
来源
MECHATRONICS ENGINEERING, COMPUTING AND INFORMATION TECHNOLOGY | 2014年 / 556-562卷
关键词
Hypersonic aircrafts; Radiation properties; Heat flow; Algorithm;
D O I
10.4028/www.scientific.net/AMM.556-562.1338
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
To research the radiation properties of heat flow around the aircrafts' surface in hypersonic flight, a fusion algorithm to calculate the radiation of flow around hypersonic aircrafts is proposed in this paper. Firstly, the algorithm use the computational fluid dynamics (CFD) to calculate the basic aerodynamic parameters of the aircrafts which are inside boundary layer, such as pressure, density, etc. Subsequently, the model of the radiation of flow around aircrafts is built by using the engineering algorithm. Then, we can build the model of the radiation properties of heat flow around the surface of the aircrafts effectively. The result can reflect the distribution of the radiation of heat flow around surfaces of the aircrafts accurately, and provide data support to study its optical detection and thermal protection.
引用
收藏
页码:1338 / 1341
页数:4
相关论文
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