临近空间高超声速飞行器红外特性建模仿真  

Infrared Simulation of Near Space Hypersonic Vehicle

作　　者：周方方[1] 张二磊[1] 陈宜峰[1] 

机构地区：[1]中国空空导弹研究院,河南洛阳471009

出　　处：《红外技术》2017年第8期746-750,共5页Infrared Technology

摘　　要：本文针对临近空间高超声速飞行器的红外特性进行建模仿真与分析。以美国X-51A的飞行器模型为例,综合考虑目标的运动状态、大气环境等的影响作用,使用FLUENT软件和SE-WORKBENCH-EO软件建立目标三维温度场模型和红外特性模型,并分析其红外特性。In this paper, research on infrared simulation of a near space hypersonic vehicle is presented. Considering X-51A as an example, the model for calculation of the 3D temperature and infrared flux of the target was developed using FLUENT and SE-WORKBENCH-EO, with comprehensive consideration of external influences, such as the impact of the atmospheric environment, the movement of the target, etc. The infrared characteristics of the target have been analyzed.

关 键 词：临近空间 高超声速飞行器 红外仿真 红外特性 

分 类 号：TN216[电子电信—物理电子学]